Storage of excess heat in cold side of heat engine

ABSTRACT

Extra heat in a closed cycle power generation system, such as a reversible closed Brayton cycle system, may be dissipated between discharge and charge cycles. An extra cooling heat exchanger may be added on the discharge cycle and disposed between a cold side heat exchanger and a compressor inlet. Additionally or alternatively, a cold thermal storage medium passing through the cold side heat exchanger may be allowed to heat up to a higher temperature during the discharge cycle than is needed on input to the charge cycle and the excess heat then dissipated to the atmosphere.

CROSS REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No. 16/260,932, filed Jan. 29, 2019, which is a Continuation of U.S. patent application Ser. No. 15/392,657, filed Dec. 28, 2016, and issued as U.S. Pat. No. 10,233,787, all of which are herein incorporated by reference in their entireties.

BACKGROUND

In a heat engine or heat pump, a heat exchanger may be employed to transfer heat between a thermal storage material and a working fluid for use with turbomachinery. The heat engine may be reversible, e.g., it also may be a heat pump, and the working fluid and heat exchanger may be used to transfer heat or cold to a plurality of thermal stores. The thermal energy within a given system may be stored in various forms and in a variety of containers, including pressure vessels and/or insulated vessels.

SUMMARY

A closed cycle system, such as a Brayton cycle system, may include at least a working fluid circulated through a closed cycle fluid path including at least two heat exchangers, a turbine, and a compressor. In some systems, one or more recuperative heat exchangers may also be included. At least two temperature reservoirs may hold thermal fluids which may be pumped through the heat exchangers, providing and/or extracting thermal energy from the working fluid. A motor/generator may be used to obtain work from the thermal energy in the system, preferably by generating electricity from mechanical energy received from the turbine.

In some cases, inefficiencies in the system may be such that excess heat must be removed from the system to close the thermodynamic cycle. Excess heat in a discharge cycle may be stored in the cold side of the heat engine prior to removal.

Example systems may include: a compressor; a recuperator; a hot side heat exchanger; a turbine; a cold side heat exchanger; a cooling heat exchanger; and a working fluid circulating in a closed cycle path through, in sequence, the compressor, the recuperator, the hot side heat exchanger, the turbine, the recuperator, the cooling heat exchanger, and the cold side heat exchanger, wherein the cooling heat exchanger is configured to remove heat from the working fluid.

Other example systems may include: a compressor; a recuperator; a hot side heat exchanger; a turbine; a cold side heat exchanger; a working fluid circulating in a closed cycle path through, in sequence, the compressor, the recuperator, the hot side heat exchanger, the turbine, the recuperator, and the cold side heat exchanger; a cold side thermal storage (“CTS”) medium; a first CTS tank; an intermediate CTS tank; a CTS heat exchanger, wherein the CTS heat exchanger is configured to remove heat from the CTS medium; a second CTS tank; a first flow path configured to flow CTS medium from the first CTS tank, through the cold side heat exchanger, and to the intermediate CTS tank; and a second flow path configured to flow CTS medium from the intermediate CTS tank, through the CTS heat exchanger, and to the second CTS tank.

Example methods may include: in a closed cycle system operating in a power generation mode, circulating a working fluid through a closed cycle fluid path including, in sequence, a compressor, a recuperator, a hot side heat exchanger, a turbine, the recuperator, and a cold side heat exchanger; flowing a cold side thermal storage (“CTS”) medium at a first variable flow rate from a first CTS tank, through the cold side heat exchanger and in thermal contact with the working fluid, and to an intermediate CTS tank; and flowing the CTS medium from the intermediate CTS tank, through a CTS heat exchanger, and to a second CTS tank, wherein the CTS heat exchanger is configured to remove heat from the CTS medium.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 schematically illustrates operation of a pumped thermal electric storage system.

FIG. 2 is a schematic flow diagram of working fluid and heat storage media of a pumped thermal system in a charge/heat pump mode.

FIG. 3 is a schematic flow diagram of working fluid and heat storage media of a pumped thermal system in a discharge/heat engine mode.

FIG. 4 is a schematic pressure and temperature diagram of the working fluid as it undergoes the charge cycle in FIG. 2.

FIG. 5 is a schematic pressure and temperature diagram of the working fluid as it undergoes the discharge cycle in FIG. 3.

FIG. 6 is a schematic perspective view of a closed working fluid system in the pumped thermal system in FIGS. 2-3.

FIG. 7 is a schematic perspective view of the pumped thermal system in FIGS. 2-3 with hot side and cold side storage tanks and a closed cycle working fluid system.

FIG. 8 shows a heat storage charge cycle for a water/molten salt system with η_(c)=0.9 and η_(t)=0.95. The dashed lines correspond to η_(c)=η_(t)=1.

FIG. 9 shows a heat storage discharge (extraction) cycle for the water/molten salt system in FIG. 8 with η_(c)=0.9 and η_(t)=0.95. The dashed lines correspond to η_(c)=η_(t)=1.

FIG. 10 shows a heat storage cycle in a pumped thermal system with variable compression ratios between the charge and discharge cycles.

FIG. 11 shows roundtrip efficiency contours for a water/salt system. The symbols ⊕ and ⊗ represent an approximate range of present large turbomachinery adiabatic efficiency values. The dashed arrows represent the direction of increasing efficiency.

FIG. 12 shows roundtrip efficiency contours for a colder storage/salt system. The symbols ⊕ and ⊗ represent an approximate range of present large turbomachinery adiabatic efficiency values.

FIG. 13 is a schematic flow diagram of working fluid and heat storage media of a pumped thermal system with a gas-gas heat exchanger for the working fluid in a charge/heat pump mode.

FIG. 14 is a schematic flow diagram of working fluid and heat storage media of a pumped thermal system with a gas-gas heat exchanger for the working fluid in a discharge/heat engine mode.

FIG. 15 is a schematic flow diagram of working fluid and heat storage media of a pumped thermal system with a gas-gas heat exchanger for the working fluid in a charge/heat pump mode with indirect heat rejection to the environment.

FIG. 16 is a schematic flow diagram of working fluid and heat storage media of a pumped thermal system with a gas-gas heat exchanger for the working fluid in a discharge/heat engine mode with indirect heat rejection to the environment.

FIG. 17 shows a heat storage charge cycle for a storage system with a gas-gas heat exchanger, a cold side storage medium capable of going down to temperatures significantly below ambient temperature and η_(c)=0.9 and η_(t)=0.95.

FIG. 18 shows a heat storage discharge cycle for a storage system with a gas-gas heat exchanger, a cold side storage medium capable of going down to temperatures significantly below ambient temperature and η_(c)=0.9 and η_(t)=0.95.

FIG. 19 is a schematic flow diagram of hot side recharging in a pumped heat cycle in solar mode with heating of a solar salt solely by solar power.

FIG. 20 is a schematic flow diagram of a pumped thermal system discharge cycle with heat rejection to ambient.

FIG. 21 is a schematic flow diagram of a pumped thermal system discharge cycle with heat rejection to an intermediate fluid circulated in a thermal bath at ambient temperature.

FIGS. 22 and 23 are pumped thermal systems with separate compressor/turbine pairs for charge and discharge modes.

FIGS. 24 and 25 show pumped thermal systems configured in a combustion heat input generation mode.

FIG. 26 is a schematic flow diagram of hot side recharging in a pumped heat cycle through heating by a combustion heat source or a waste heat source.

FIG. 27 shows an example of a pumped thermal system with pressure regulated power control.

FIG. 28 shows an example of a pumped thermal system with a pressure encased generator.

FIG. 29 is an example of variable stators in a compressor/turbine pair.

FIG. 30 shows a computer system that is programmed to implement various methods and/or regulate various systems of the present disclosure.

FIG. 31 illustrates a thermodynamic pressure-temperature chart for a charge cycle, according to an example embodiment.

FIG. 32 illustrates a thermodynamic pressure-temperature chart for a discharge cycle, according to an example embodiment.

FIG. 33 illustrates a Brayton system in discharging mode with cold side heat storage, according to an example embodiment.

FIG. 34 illustrates a Brayton system in discharging mode with cold side heat storage, according to an example embodiment.

FIG. 35 illustrates a method for storing and dissipating heat from cold side heat storage, according to an example embodiment.

DETAILED DESCRIPTION

While various embodiments of the invention have been shown and described herein, it will be obvious to those skilled in the art that such embodiments are provided by way of example only. Numerous variations, changes, and substitutions may occur to those skilled in the art without departing from the invention. It should be understood that various alternatives to the embodiments of the invention described herein may be employed. It shall be understood that different aspects of the invention can be appreciated individually, collectively, or in combination with each other.

It is to be understood that the terminology used herein is used for the purpose of describing specific embodiments, and is not intended to limit the scope of the present invention. It should be noted that as used herein, the singular forms of “a”, “an” and “the” include plural references unless the context clearly dictates otherwise. In addition, unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs.

While preferable embodiments of the present invention are shown and described herein, it will be obvious to those skilled in the art that such embodiments are provided by way of example only. Numerous variations, changes, and substitutions will now occur to those skilled in the art without departing from the invention. It should be understood that various alternatives to the embodiments of the invention described herein may be employed in practicing the invention. It is intended that the following claims define the scope of the invention and that methods and structures within the scope of these claims and their equivalents be covered thereby.

The term “reversible,” as used herein, generally refers to a process or operation that can be reversed via infinitesimal changes in some property of the process or operation without substantial entropy production (e.g., dissipation of energy). A reversible process may be approximated by a process that is at thermodynamic equilibrium. In some examples, in a reversible process, the direction of flow of energy is reversible. As an alternative, or in addition to, the general direction of operation of a reversible process (e.g., the direction of fluid flow) can be reversed, such as, e.g., from clockwise to counterclockwise, and vice versa.

The term “sequence,” as used herein, generally refers to elements (e.g., unit operations) in order. Such order can refer to process order, such as, for example, the order in which a fluid flows from one element to another. In an example, a compressor, heat storage unit and turbine in sequence includes the compressor upstream of the heat exchange unit, and the heat exchange unit upstream of the turbine. In such a case, a fluid can flow from the compressor to the heat exchange unit and from the heat exchange unit to the turbine. A fluid flowing through unit operations in sequence can flow through the unit operations sequentially. A sequence of elements can include one or more intervening elements. For example, a system comprising a compressor, heat storage unit and turbine in sequence can include an auxiliary tank between the compressor and the heat storage unit. A sequence of elements can be cyclical.

I. OVERVIEW

A closed cycle system, such as a closed Brayton cycle system, may use a generator/motor connected to a turbine and a compressor which act on a working fluid circulating in the system. Examples of working fluids include air, argon, carbon dioxide, or gaseous mixtures. A closed cycle system may have a hot side and/or a cold side. Each side may include a heat exchanger coupled to one or more cold storage containers and/or one or more hot storage containers. Preferably, the heat exchangers may be arranged as counterflow heat exchangers for higher thermal efficiency. Liquid thermal storage medium be utilized and may include, for example, liquids that are stable at high temperatures, such as molten nitrate salt or solar salt, or liquids that are stable at low temperatures, such as glycols or alkanes such as hexane. For an example molten salt and hexane system, the hot side molten salt may include a hot storage at approximately 565° C. and a cold storage at approximately 290° C. and the cold side hexane may include a hot storage at approximately 35° C. and a cold storage at approximately −60° C.

If polytropic efficiencies turbomachinery are less than 100% in a Brayton cycle power generation system, extra heat may need to be dissipated between discharge and charge cycles. In one embodiment, an extra cooling heat exchanger may be added on the discharge cycle and disposed between the cold side heat exchanger and the turbine outlet. In the cooling heat exchanger, the working fluid may exchange heat with another fluid such as water or Therminol® to carry away the excess heat. In another embodiment, in place of having another heat exchanger in the working fluid path, a cold thermal storage (“CTS”) medium passing through the cold side heat exchanger may be allowed to heat up to a higher temperature during the discharge cycle than is needed on input to the charge cycle. This hotter CTS medium may then be stored in an intermediate tank. The hotter CTS medium may then be put through an intermediate cooling mechanism and returned to a final CTS tank, ready to be used in the charge cycle. This embodiment has an advantage over the prior embodiment in that (i) it eliminates the need for an additional working fluid cooling heat exchanger and different heat exchange fluid and (ii) it decouples the instantaneous cooling power needed from the immediate heat dissipation needs in the discharge cycle. Specifically, waste heat is being stored in the CTS medium, therefore the overall system can use a smaller amount of cooling power than required in the prior embodiment by dissipating the same number of Joules but over a larger amount of time. In further embodiments, the working fluid temperature in the cold side heat exchanger may be above the boiling temperature of CTS medium at ambient pressure. In one embodiment, the flow of CTS medium through the cold side heat exchanger can be increased such that the same amount of cooling is accomplished but the CTS medium is not allowed to reach its boiling point. In another embodiment, the CTS medium may be allowed to evaporate, taking advantage of its latent heat of vaporization and then re-condensed in subsequent infrastructure.

II. ILLUSTRATIVE REVERSIBLE HEAT ENGINE Pumped Thermal Systems

The disclosure provides pumped thermal systems capable of storing electrical energy and/or heat, and releasing energy (e.g., producing electricity) at a later time. The pumped thermal systems of the disclosure may include a heat engine, and a heat pump (or refrigerator). In some cases, the heat engine can be operated in reverse as a heat pump. In some cases, the heat engine can be operated in reverse as a refrigerator. Any description of heat pump/heat engine systems or refrigerator/heat engine systems capable of reverse operation herein may also be applied to systems comprising separate and/or a combination of separate and reverse-operable heat engine system(s), heat pump system(s) and/or refrigerator system(s). Further, as heat pumps and refrigerators share the same operating principles (albeit with differing objectives), any description of configurations or operation of heat pumps herein may also be applied to configurations or operation of refrigerators, and vice versa.

Systems of the present disclosure can operate as heat engines or heat pumps (or refrigerators). In some situations, systems of the disclosure can alternately operate as heat engines and heat pumps. In some examples, a system can operate as a heat engine to generate power, and subsequently operate as a heat pump to store energy, or vice versa. Such systems can alternately and sequentially operate as heat engines as heat pumps. In some cases, such systems reversibly or substantially reversibly operate as heat engines as heat pumps.

Reference will now be made to the figures, wherein like numerals refer to like parts throughout. It will be appreciated that the figures and features therein are not necessarily drawn to scale.

FIG. 1 schematically illustrates operating principles of pumped thermal electric storage using a heat pump/heat engine electricity storage system. Electricity may be stored in the form of thermal energy of two materials or media at different temperatures (e.g., thermal energy reservoirs comprising heat storage fluids or thermal storage media) by using a combined heat pump/heat engine system. In a charging or heat pump mode, work may be consumed by the system for transferring heat from a cold material or medium to a hot material or medium, thus lowering the temperature (e.g., sensible energy) of the cold material and increasing the temperature (i.e., sensible energy) of the hot material. In a discharging or heat engine mode, work may be produced by the system by transferring heat from the hot material to the cold material, thus lowering the temperature (i.e., sensible energy) of the hot material and increasing the temperature (i.e., sensible energy) of the cold material. The system may be configured to ensure that the work produced by the system on discharge is a favorable fraction of the energy consumed on charge. The system may be configured to achieve high roundtrip efficiency, defined herein as the work produced by the system on discharge divided by the work consumed by the system on charge. Further, the system may be configured to achieve the high roundtrip efficiency using components of a desired (e.g., acceptably low) cost. Arrows H and W in FIG. 1 represent directions of heat flow and work, respectively.

Heat engines, heat pumps and refrigerators of the disclosure may involve a working fluid to and from which heat is transferred while undergoing a thermodynamic cycle. The heat engines, heat pumps and refrigerators of the disclosure may operate in a closed cycle. Closed cycles allow, for example, a broader selection of working fluids, operation at elevated cold side pressures, operation at lower cold side temperatures, improved efficiency, and reduced risk of turbine damage. One or more aspects of the disclosure described in relation to systems having working fluids undergoing closed cycles may also be applied to systems having working fluids undergoing open cycles.

In one example, the heat engines may operate on a Brayton cycle and the heat pumps/refrigerators may operate on a reverse Brayton cycle (also known as a gas refrigeration cycle). Other examples of thermodynamic cycles that the working fluid may undergo or approximate include the Rankine cycle, the ideal vapor-compression refrigeration cycle, the Stirling cycle, the Ericsson cycle or any other cycle advantageously employed in concert with heat exchange with heat storage fluids of the disclosure.

The working fluid can undergo a thermodynamic cycle operating at one, two or more pressure levels. For example, the working fluid may operate in a closed cycle between a low pressure limit on a cold side of the system and a high pressure limit on a hot side of the system. In some implementations, a low pressure limit of about 10 atmospheres (atm) or greater can be used. In some instances, the low pressure limit may be at least about 1 atm, at least about 2 atm, at least about 5 atm, at least about 10 atm, at least about 15 atm, at least about 20 atm, at least about 30 atm, at least about 40 atm, at least about 60 atm, at least about 80 atm, at least about 100 atm, at least about 120 atm, at least about 160 atm, or at least about 200 atm, 500 atm, 1000 atm, or more. In some instances, a sub-atmospheric low pressure limit may be used. For example, the low pressure limit may be less than about 0.1 atm, less than about 0.2 atm, less than about 0.5 atm, or less than about 1 atm. In some instances, the low pressure limit may be about 1 atmosphere (atm). In the case of a working fluid operating in an open cycle, the low pressure limit may be about 1 atm or equal to ambient pressure.

In some cases, the value of the low pressure limit may be selected based on desired power output and/or power input requirements of the thermodynamic cycle. For example, a pumped thermal system with a low pressure limit of about 10 atm may be able to provide a power output comparable to an industrial gas turbine with ambient (1 atm) air intake. The value of the low pressure limit may also be subject to cost/safety tradeoffs. Further, the value of the low pressure limit may be limited by the value of the high pressure limit, the operating ranges of the hot side and cold side heat storage media (e.g., pressure and temperature ranges over which the heat storage media are stable), pressure ratios and operating conditions (e.g., operating limits, optimal operating conditions, pressure drop) achievable by turbomachinery and/or other system components, or any combination thereof. The high pressure limit may be determined in accordance with these system constraints. In some instances, higher values of the high pressure limit may lead to improved heat transfer between the working fluid and the hot side storage medium.

Working fluids used in pumped thermal systems may include air, argon, other noble gases, carbon dioxide, hydrogen, oxygen, or any combination thereof, and/or other fluids in gaseous, liquid, critical, or supercritical state (e.g., supercritical CO₂). The working fluid can be a gas or a low viscosity liquid (e.g., viscosity below about 500×10⁻⁶ Poise at 1 atm), satisfying the requirement that the flow be continual. In some implementations, a gas with a high specific heat ratio may be used to achieve higher cycle efficiency than a gas with a low specific heat ratio. For example, argon (e.g., specific heat ratio of about 1.66) may be used to substitute air (e.g., specific heat ratio of about 1.4). In some cases, the working fluid may be a blend of one, two, three or more fluids. In one example, helium (having a high thermal conductivity and a high specific heat) may be added to the working fluid (e.g., argon) to improve heat transfer rates in heat exchangers.

Pumped thermal systems herein may utilize heat storage media or materials, such as one or more heat storage fluids. The heat storage media can be gases or low viscosity liquids, satisfying the requirement that the flow be continual. The systems may utilize a first heat storage medium on a hot side of the system (“hot side thermal storage (HTS) medium” or “HTS” herein) and a second heat storage medium on a cold side of the system (“cold side thermal storage (CTS) medium” or “CTS” herein). The thermal storage media (e.g., low viscosity liquids) can have high heat capacities per unit volume (e.g., heat capacities above about 1400 Joule (kilogram Kelvin)⁻¹) and high thermal conductivities (e.g., thermal conductivities above about 0.7 Watt (meter Kelvin)⁻¹). In some implementations, several different thermal storage media (also “heat storage media” herein) on either the hot side, cold side or both the hot side and the cold side may be used.

The operating temperatures of the hot side thermal storage medium can be in the liquid range of the hot side thermal storage medium, and the operating temperatures of the cold side thermal storage medium can be in the liquid range of the cold side thermal storage medium. In some examples, liquids may enable a more rapid exchange of large amounts of heat by convective counter-flow than solids or gases. Thus, in some cases, liquid HTS and CTS media may advantageously be used. Pumped thermal systems utilizing thermal storage media herein may advantageously provide a safe, non-toxic and geography-independent energy (e.g., electricity) storage alternative.

In some implementations, the hot side thermal storage medium can be a molten salt or a mixture of molten salts. Any salt or salt mixture that is liquid over the operating temperature range of the hot side thermal storage medium may be employed. Molten salts can provide numerous advantages as thermal energy storage media, such as low vapor pressure, lack of toxicity, chemical stability, low chemical reactivity with typical steels (e.g., melting point below the creep temperature of steels, low corrosiveness, low capacity to dissolve iron and nickel), and low cost. In one example, the HTS is a mixture of sodium nitrate and potassium nitrate. In some examples, the HTS is a eutectic mixture of sodium nitrate and potassium nitrate. In some examples, the HTS is a mixture of sodium nitrate and potassium nitrate having a lowered melting point than the individual constituents, an increased boiling point than the individual constituents, or a combination thereof. Other examples include potassium nitrate, calcium nitrate, sodium nitrate, sodium nitrite, lithium nitrate, mineral oil, or any combination thereof. Further examples include any gaseous (including compressed gases), liquid or solid media (e.g., powdered solids) having suitable (e.g., high) thermal storage capacities and/or capable of achieving suitable (e.g., high) heat transfer rates with the working fluid. For example, a mix of 60% sodium nitrate and 40% potassium nitrate (also referred to as a solar salt in some situations) can have a heat capacity of approximately 1500 Joule (Kelvin mole)⁻¹ and a thermal conductivity of approximately 0.75 Watt (meter Kelvin)⁻¹ within a temperature range of interest. The hot side thermal storage medium may be operated in a temperature range that structural steels can handle.

In some cases, liquid water at temperatures of about 0° C. to 100° C. (about 273 K-373 K) and a pressure of about 1 atm may be used as the cold side thermal storage medium. Due to a possible explosion hazard associated with presence of steam at or near the boiling point of water, the operating temperature can be kept below about 100° C. or less while maintaining an operating pressure of 1 atm (i.e., no pressurization). In some cases, the temperature operating range of the cold side thermal storage medium may be extended (e.g., to −30° C. to 100° C. at 1 atm) by using a mixture of water and one or more antifreeze compounds (e.g., ethylene glycol, propylene glycol, or glycerol).

As described in greater detail elsewhere herein, improved storage efficiency may be achieved by increasing the temperature difference at which the system operates, for example, by using a cold side heat storage fluid capable of operating at lower temperatures. In some examples, the cold side thermal storage media may comprise hydrocarbons, such as, for example, alkanes (e.g., hexane or heptane), alkenes, alkynes, aldehydes, ketones, carboxylic acids (e.g., HCOOH), ethers, cycloalkanes, aromatic hydrocarbons, alcohols (e.g., butanol), other type(s) of hydrocarbon molecules, or any combinations thereof. In some cases, the cold side thermal storage medium can be hexane (e.g., n-hexane). Hexane has a wide liquid range and can remain fluid (i.e., runny) over its entire liquid range (−94° C. to 68° C. at 1 atm). Hexane's low temperature properties are aided by its immiscibility with water. Other liquids, such as, for example, ethanol or methanol can become viscous at the low temperature ends of their liquid ranges due to pre-crystallization of water absorbed from air. In some cases, the cold side thermal storage medium can be heptane (e.g., n-heptane). Heptane has a wide liquid range and can remain fluid (i.e., runny) over its entire liquid range (−91° C. to 98° C. at 1 atm). Heptane's low temperature properties are aided by its immiscibility with water. At even lower temperatures, other heat storage media can be used, such as, for example, isohexane (2-methylpentane). In some examples, cryogenic liquids having boiling points below about −150° C. (123 K) or about −180° C. (93.15 K) may be used as cold side thermal storage media (e.g., propane, butane, pentane, nitrogen, helium, neon, argon and krypton, air, hydrogen, methane, or liquefied natural gas). In some implementations, choice of cold side thermal storage medium may be limited by the choice of working fluid. For example, when a gaseous working fluid is used, a liquid cold side thermal storage medium having a liquid temperature range at least partially or substantially above the boiling point of the working fluid may be required.

In some cases, the operating temperature range of CTS and/or HTS media can be changed by pressurizing (i.e., raising the pressure) or evacuating (i.e., lowering the pressure) the tanks and thus changing the temperature at which the storage media undergo phase transitions (e.g., going from liquid to solid, or from liquid to gas).

In some cases, the hot side and the cold side heat storage fluids of the pumped thermal systems are in a liquid state over at least a portion of the operating temperature range of the energy storage device. The hot side heat storage fluid may be liquid within a given range of temperatures. Similarly, the cold side heat storage fluid may be liquid within a given range of temperatures. The heat storage fluids may be heated, cooled or maintained to achieve a suitable operating temperature prior to, during or after operation.

Pumped thermal systems of the disclosure may cycle between charged and discharged modes. In some examples, the pumped thermal systems can be fully charged, partially charged or partially discharged, or fully discharged. In some cases, cold side heat storage may be charged (also “recharged” herein) independently from hot side heat storage. Further, in some implementations, charging (or some portion thereof) and discharging (or some portion thereof) can occur simultaneously. For example, a first portion of a hot side heat storage may be recharged while a second portion of the hot side heat storage together with a cold side heat storage are being discharged.

The pumped thermal systems may be capable of storing energy for a given amount of time. In some cases, a given amount of energy may be stored for at least about 1 second, at least about 30 seconds, at least about 1 minute, at least about 5 minutes, at least about 30 minutes, at least about 1 hour, at least about 2 hours, at least about 3 hours, at least about 4 hours, at least about 5 hours, at least about 6 hours, at least about 7 hours, at least about 8 hours, at least about 9 hours, at least about 10 hours, at least about 12 hours at least about 14 hours, at least about 16 hours, at least about 18 hours, at least about 20 hours, at least about 22 hours, at least about 24 hours (1 day), at least about 2 days, at least about 4 days, at least about 6 days, at least about 8 days, at least about 10 days, 20 days, 30 days, 60 days, 100 days, 1 year or more.

Pumped thermal systems of the disclosure may be capable of storing/receiving input of, and/or extracting/providing output of a substantially large amount of energy and/or power for use with power generation systems (e.g., intermittent power generation systems such as wind power or solar power), power distribution systems (e.g. electrical grid), and/or other loads or uses in grid-scale or stand-alone settings. During a charge mode of a pumped thermal system, electric power received from an external power source (e.g., a wind power system, a solar photovoltaic power system, an electrical grid etc.) can be used operate the pumped thermal system in a heat pump mode (i.e., transferring heat from a low temperature reservoir to a high temperature reservoir, thus storing energy). During a discharge mode of the pumped thermal system, the system can supply electric power to an external power system or load (e.g., one or more electrical grids connected to one or more loads, a load, such as a factory or a power-intensive process, etc.) by operating in a heat engine mode (i.e., transferring heat from a high temperature reservoir to a low temperature reservoir, thus extracting energy). As described elsewhere herein, during charge and/or discharge, the system may receive or reject thermal power, including, but not limited to electromagnetic power (e.g., solar radiation) and thermal power (e.g., sensible energy from a medium heated by solar radiation, heat of combustion etc.).

In some implementations, the pumped thermal systems are grid-synchronous. Synchronization can be achieved by matching speed and frequency of motors/generators and/or turbomachinery of a system with the frequency of one or more grid networks with which the system exchanges power. For example, a compressor and a turbine can rotate at a given, fixed speed (e.g., 3600 revolutions per minute (rpm)) that is a multiple of grid frequency (e.g., 60 hertz (Hz)). In some cases, such a configuration may eliminate the need for additional power electronics. In some implementations, the turbomachinery and/or the motors/generators are not grid synchronous. In such cases, frequency matching can be accomplished through the use of power electronics. In some implementations, the turbomachinery and/or the motors/generators are not directly grid synchronous but can be matched through the use of gears and/or a mechanical gearbox. As described in greater detail elsewhere herein, the pumped thermal systems may also be rampable. Such capabilities may enable these grid-scale energy storage systems to operate as peaking power plants and/or as a load following power plants. In some cases, the systems of the disclosure may be capable of operating as base load power plants.

Pumped thermal systems can have a given power capacity. In some cases, power capacity during charge may differ from power capacity during discharge. For example, each system can have a charge and/or discharge power capacity of less than about 1 megawatt (MW), at least about 1 megawatt, at least about 2 MW, at least about 3 MW, at least about 4 MW, at least about 5 MW, at least about 6 MW, at least about 7 MW, at least about 8 MW, at least about 9 MW, at least about 10 MW, at least about 20 MW, at least about 30 MW, at least about 40 MW, at least about 50 MW, at least about 75 MW, at least about 100 MW, at least about 200 MW, at least about 500 MW, at least about 1 gigawatt (GW), at least about 2 GW, at least about 5 GW, at least about 10 GW, at least about 20 GW, at least about 30 GW, at least about 40 GW, at least about 50 GW, at least about 75 GW, at least about 100 GW, or more.

Pumped thermal systems can have a given energy storage capacity. In one example, a pumped thermal system is configured as a 100 MW unit operating for 10 hours. In another example, a pumped thermal system is configured as a 1 GW plant operating for 12 hours. In some instances, the energy storage capacity can be less than about 1 megawatt hour (MWh), at least about 1 megawatt hour, at least about 10 MWh, at least about 100 MWh, at least about 1 gigawatt hour (GWh), at least about 5 GWh, at least about 10 GWh, at least about 20 GWh, at least 50 GWh, at least about 100 GWh, at least about 200 GWh, at least about 500 GWh, at least about 700 GWh, at least about 1000 GWh, or more.

In some cases, a given power capacity may be achieved with a given size, configuration and/or operating conditions of the heat engine/heat pump cycle. For example, size of turbomachinery, ducts, heat exchangers, or other system components may correspond to a given power capacity.

In some implementations, a given energy storage capacity may be achieved with a given size and/or number of hot side thermal storage tanks and/or cold side thermal storage tanks. For example, the heat engine/heat pump cycle can operate at a given power capacity for a given amount of time set by the heat storage capacity of the system or plant. The number and/or heat storage capacity of the hot side thermal storage tanks may be different from the number and/or heat storage capacity of the cold side thermal storage tanks. The number of tanks may depend on the size of individual tanks. The size of hot side storage tanks may differ from the size of cold side thermal storage tanks. In some cases, the hot side thermal storage tanks, the hot side heat exchanger and the hot side thermal storage medium may be referred to as a hot side heat (thermal) storage unit. In some cases, the cold side thermal storage tanks, the cold side heat exchanger and the cold side thermal storage medium may be referred to as a cold side heat (thermal) storage unit.

A pumped thermal storage facility can include any suitable number of hot side storage tanks, such as at least about 2, at least about 4, at least about 10, at least about 50, at least about 100, at least about 500, at least about 1,000, at least about 5,000, at least about 10,000, and the like. In some examples, a pumped thermal storage facility includes 2, 3, 4, 5, 6, 7, 8, 9, 10, 15, 20, 30, 40, 50, 60, 70, 80, 90, 100, 200, 300, 400, 500, 600, 700, 800, 900, 1,000 or more hot side tanks.

A pumped thermal storage facility can also include any suitable number of cold side storage tanks, such as at least about 2, at least about 4, at least about 10, at least about 50, at least about 100, at least about 500, at least about 1,000, at least about 5,000, at least about 10,000, and the like. In some examples, a pumped thermal storage facility includes 2, 3, 4, 5, 6, 7, 8, 9, 10, 15, 20, 30, 40, 50, 60, 70, 80, 90, 100, 200, 300, 400, 500, 600, 700, 800, 900, 1,000 or more cold side tanks.

Pumped Thermal Storage Cycles

An aspect of the disclosure relates to pumped thermal systems operating on pumped thermal storage cycles. In some examples, the cycles allow electricity to be stored as heat (e.g., in the form of a temperature differential) and then converted back to electricity through the use of at least two pieces of turbomachinery, a compressor and a turbine. The compressor consumes work and raises the temperature and pressure of a working fluid (WF). The turbine produces work and lowers the temperature and pressure of the working fluid. In some examples, more than one compressor and more than one turbine is used. In some cases, the system can include at least 1, at least 2, at least 3, at least 4, or at least 5 compressors. In some cases, the system can include at least 1, at least 2, at least 3, at least 4, or at least 5 turbines. The compressors may be arranged in series or in parallel. The turbines may be arranged in series or in parallel.

FIGS. 2 and 3 are schematic flow diagrams of working fluid and heat storage media of an exemplary pumped thermal system in a charge/heat pump mode and in a discharge/heat engine mode, respectively. The system may be idealized for simplicity of explanation so that there are no losses (i.e., entropy generation) in either the turbomachinery or heat exchangers. The system can include a working fluid 20 (e.g., argon gas) flowing in a closed cycle between a compressor 1, a hot side heat exchanger 2, a turbine 3 and a cold side heat exchanger 4. Fluid flow paths/directions for the working fluid 20 (e.g., a gas), a hot side thermal storage (HTS) medium 21 (e.g., a low viscosity liquid) and a cold side thermal storage (CTS) medium 22 (e.g., a low viscosity liquid) are indicated by arrows.

FIGS. 4 and 5 are schematic pressure and temperature diagrams of the working fluid 20 as it undergoes the charge cycles in FIGS. 2 and 3, respectively, once again simplified in the approximation of no entropy generation. Normalized pressure is shown on the y-axes and temperature is shown on the x-axes. The direction of processes taking place during the cycles is indicated with arrows, and the individual processes taking place in the compressor 1, the hot side CFX 2, the turbine 3 and the cold side CFX 4 are indicated on the diagram with their respective numerals.

The heat exchangers 2 and 4 can be configured as counter-flow heat exchangers (CFXs), where the working fluid flows in one direction and the substance it is exchanging heat with is flowing in the opposite direction. In an ideal counter-flow heat exchanger with correctly matched flows (i.e., balanced capacities or capacity flow rates), the temperatures of the working fluid and thermal storage medium flip (i.e., the counter-flow heat exchanger can have unity effectiveness).

The counter-flow heat exchangers 2 and 4 can be designed and/or operated to reduce entropy generation in the heat exchangers to negligible levels compared to entropy generation associated with other system components and/or processes (e.g., compressor and/or turbine entropy generation). In some cases, the system may be operated such that entropy generation in the system is minimized. For example, the system may be operated such that entropy generation associated with heat storage units is minimized. In some cases, a temperature difference between fluid elements exchanging heat can be controlled during operation such that entropy generation in hot side and cold side heat storage units is minimized. In some instances, the entropy generated in the hot side and cold side heat storage units is negligible when compared to the entropy generated by the compressor, the turbine, or both the compressor and the turbine. In some instances, entropy generation associated with heat transfer in the heat exchangers 2 and 4 and/or entropy generation associated with operation of the hot side storage unit, the cold side storage unit or both the hot side and cold side storage units can be less than about 50%, less than about 25%, less than about 20%, less than about 15%, less than about 10%, less than about 5%, less than about 4%, less than about 3%, less than about 2%, or less than about 1% of the total entropy generated within the system (e.g., entropy generated by the compressor 1, the hot side heat exchanger 2, the turbine 3, the cold side heat exchanger 4 and/or other components described herein, such as, for example, a recuperator). For example, entropy generation can be reduced or minimized if the two substances exchanging heat do so at a local temperature differential ΔT→0 (i.e., when the temperature difference between any two fluid elements that are in close thermal contact in the heat exchanger is small). In some examples, the temperature differential ΔT between any two fluid elements that are in close thermal contact may be less than about 300 Kelvin (K), less than about 200 K, less than about 100 K, less than about 75 K, less than about 50 K, less than about 40 K, less than about 30 K, less than about 20 K, less than about 10 K, less than about 5 K, less than about 3 K, less than about 2 K, or less than about 1 K. In another example, entropy generation associated with pressure drop can be reduced or minimized by suitable design. In some examples, the heat exchange process can take place at a constant or near-constant pressure. Alternatively, a non-negligible pressure drop may be experienced by the working fluid and/or one or more thermal storage media during passage through a heat exchanger. Pressure drop in heat exchangers may be controlled (e.g., reduced or minimized) through suitable heat exchanger design. In some examples, the pressure drop across each heat exchanger may be less than about 20% of inlet pressure, less than about 10% of inlet pressure, less than about 5% of inlet pressure, less than about 3% of inlet pressure, less than about 2% of inlet pressure, less than about 1% of inlet pressure, less than about 0.5% of inlet pressure, less than about 0.25% of inlet pressure, or less than about 0.1% of inlet pressure.

Upon entering the heat exchanger 2, the temperature of the working fluid can either increase (taking heat from the HTS medium 21, corresponding to the discharge mode in FIGS. 3 and 5) or decrease (giving heat to the HTS medium 21, corresponding to the charge mode in FIGS. 2 and 4), depending on the temperature of the HTS medium in the heat exchanger relative the temperature of the working fluid. Similarly, upon entering the heat exchanger 4, the temperature of the working fluid can either increase (taking heat from the CTS medium 22, corresponding to the charge mode in FIGS. 2 and 4) or decrease (giving heat to the CTS medium 22, corresponding to the discharge mode in FIGS. 3 and 5), depending on the temperature of the CTS medium in the heat exchanger relative the temperature of the working fluid.

As described in more detail with reference to the charge mode in FIGS. 2 and 4, the heat addition process in the cold side CFX 4 can take place over a different range of temperatures than the heat removal process in the hot side CFX 2. Similarly, in the discharge mode in FIGS. 3 and 5, the heat rejection process in the cold side CFX 4 can take place over a different range of temperatures than the heat addition process in the hot side CFX 2. At least a portion of the temperature ranges of the hot side and cold side heat exchange processes may overlap during charge, during discharge, or during both charge and discharge.

As used herein, the temperatures T₀, T₁, T₀ ⁺ and T₁ ⁺ are so named because T₀ ⁺, T₁ ⁺ are the temperatures achieved at the exit of a compressor with a given compression ratio r, adiabatic efficiency η_(c) and inlet temperatures of T₀, T₁ respectively. The examples in FIGS. 2, 3, 4 and 5 can be idealized examples where η_(c)=1 and where adiabatic efficiency of the turbine η_(t) also has the value η_(t)=1.

With reference to the charge mode shown in FIGS. 2 and 4, the working fluid 20 can enter the compressor 1 at position 30 at a pressure P and a temperature T (e.g., at T₁, P₂). As the working fluid passes through the compressor, work W₁ is consumed by the compressor to increase the pressure and temperature of the working fluid (e.g., to T₁ ⁺, P₁), as indicated by P↑ and T↑ at position 31. In the charge mode, the temperature T₁ ⁺ of the working fluid exiting the compressor and entering the hot side CFX 2 at position 31 is higher than the temperature of the HTS medium 21 entering the hot side CFX 2 at position 32 from a second hot side thermal storage tank 7 at a temperature T₀ ⁺ (i.e., T₀ ⁺<T₁ ⁺). As these two fluids pass in thermal contact with each other in the heat exchanger, the working fluid's temperature decreases as it moves from position 31 position 34, giving off heat Q₁ to the HTS medium, while the temperature of the HTS medium in turn increases as it moves from position 32 to position 33, absorbing heat Q₁ from the working fluid. In an example, the working fluid exits the hot side CFX 2 at position 34 at the temperature T₀ ⁺ and the HTS medium exits the hot side CFX 2 at position 33 into a first hot side thermal storage tank 6 at the temperature T₁ ⁺. The heat exchange process can take place at a constant or near-constant pressure such that the working fluid exits the hot side CFX 2 at position 34 at a lower temperature but same pressure P₁, as indicated by P and T↓ at position 34. Similarly, the temperature of the HTS medium 21 increases in the hot side CFX 2, while its pressure can remain constant or near-constant.

Upon exiting the hot side CFX 2 at position 34 (e.g., at T₀ ⁺, P₁), the working fluid 20 undergoes expansion in the turbine 3 before exiting the turbine at position 35. During the expansion, the pressure and temperature of the working fluid decrease (e.g., to T₀, P₂), as indicated by P↓ and T↓ at position 35. The magnitude of work W₂ generated by the turbine depends on the enthalpy of the working fluid entering the turbine and the degree of expansion. In the charge mode, heat is removed from the working fluid between positions 31 and 34 (in the hot side CFX 2) and the working fluid is expanded back to the pressure at which it initially entered the compressor at position 30 (e.g., P₂). The compression ratio (e.g., P₁/P₂) in the compressor 1 being equal to the expansion ratio in the turbine 3, and the enthalpy of the gas entering the turbine being lower than the enthalpy of the gas exiting the compressor, the work W₂ generated by the turbine 3 is smaller than the work W₁ consumed by the compressor 1 (i.e., W₂<W₁).

Because heat was taken out of the working fluid in the hot side CFX 2, the temperature T₀ at which the working fluid exits the turbine at position 35 is lower than the temperature T₁ at which the working fluid initially entered the compressor at position 30. To close the cycle (i.e., to return the pressure and temperature of the working fluid to their initial values T₁, P₂ at position 30), heat Q₂ is added to the working fluid from the CTS medium 22 in the cold side CFX 4 between positions 35 and 30 (i.e., between the turbine 3 and the compressor 1). In an example, the CTS medium 22 enters the cold side CFX 4 at position 36 from a first cold side thermal storage tank 8 at the temperature T₁ and exits the cold side CFX 4 at position 37 into a second cold side thermal storage tank 9 at the temperature T₀, while the working fluid 20 enters the cold side CFX 4 at position 35 at the temperature T₀ and exits the cold side CFX 4 at position 30 at the temperature T₁. Again, the heat exchange process can take place at a constant or near-constant pressure such that the working fluid exits the cold side CFX 2 at position 30 at a higher temperature but same pressure P₂, as indicated by P and T↑ at position 30. Similarly, the temperature of the CTS medium 22 decreases in the cold side CFX 2, while its pressure can remain constant or near-constant.

During charge, the heat Q₂ is removed from the CTS medium and the heat Q₁ is added to the HTS medium, wherein Q₁>Q₂. A net amount of work W₁−W₂ is consumed, since the work W₁ used by the compressor is greater than the work W₂ generated by the turbine. A device that consumes work while moving heat from a cold body or thermal storage medium to a hot body or thermal storage medium is a heat pump; thus, the pumped thermal system in the charge mode operates as a heat pump.

In an example, the discharge mode shown in FIGS. 3 and 5 can differ from the charge mode shown in FIGS. 2 and 4 in the temperatures of the thermal storage media being introduced into the heat exchangers. The temperature at which the HTS medium enters the hot side CFX 2 at position 32 is T₁ ⁺ instead of T₀ ⁺, and the temperature of the CTS medium entering the cold side CFX 4 at position 36 is T₀ instead of T₁. During discharge, the working fluid enters the compressor at position 30 at T₀ and P₂, exits the compressor at position 31 at T₀ ⁺<T₁ ⁺ and P₁, absorbs heat from the HTS medium in the hot side CFX 2, enters the turbine 3 at position 34 at T₁ ⁺ and P₁, exits the turbine at position 35 at T₁>T₀ and P₂, and finally rejects heat to the CTS medium in the cold side CFX 4, returning to its initial state at position 30 at T₀ and P₂.

The HTS medium at temperature T₁ ⁺ can be stored in a first hot side thermal storage tank 6, the HTS medium at temperature T₀ ⁺ can be stored in a second hot side thermal storage tank 7, the CTS medium at temperature T₁ can be stored in a first cold side thermal storage tank 8, and the CTS medium at temperature T₀ can be stored in a second cold side thermal storage tank 9 during both charge and discharge modes. In one implementation, the inlet temperature of the HTS medium at position 32 can be switched between T₁ ⁺ and T₀ ⁺ by switching between tanks 6 and 7, respectively. Similarly, the inlet temperature of the CTS medium at position 36 can be switched between T₁ and T₀ by switching between tanks 8 and 9, respectively. Switching between tanks can be achieved by including a valve or a system of valves (e.g., valve systems 12 and 13 in FIG. 7) for switching connections between the hot side heat exchanger 2 and the hot side tanks 6 and 7, and/or between the cold side heat exchanger 4 and the cold side tanks 8 and 9 as needed for the charge and discharge modes. In some implementations, connections may be switched on the working fluid side instead, while the connections of storage tanks 6, 7, 8 and 9 to the heat exchangers 2 and 4 remain static. In some examples, flow paths and connections to the heat exchangers may depend on the design (e.g., shell-and-tube) of each heat exchanger. In some implementations, one or more valves can be used to switch the direction of both the working fluid and the heat storage medium through the counter-flow heat exchanger on charge and discharge. Such configurations may be used, for example, due to high thermal storage capacities of the heat exchanger component, to decrease or eliminate temperature transients, or a combination thereof. In some implementations, one or more valves can be used to switch the direction of only the working fluid, while the direction of the HTS or CTS can be changed by changing the direction of pumping, thereby maintaining the counter-flow configuration. In some implementations, different valve configurations may be used for the HTS and the CTS. Further, any combination of the valve configurations herein may be used. For example, the system may be configured to operate using different valve configurations in different situations (e.g., depending on system operating conditions).

In the discharge mode shown in FIGS. 3 and 5, the working fluid 20 can enter the compressor 1 at position 30 at a pressure P and a temperature T (e.g., at T₀, P₂). As the working fluid passes through the compressor, work W₁ is consumed by the compressor to increase the pressure and temperature of the working fluid (e.g., to T₀ ⁺, P₁), as indicated by P↑ and T↑ at position 31. In the discharge mode, the temperature T₀ ⁺ of the working fluid exiting the compressor and entering the hot side CFX 2 at position 31 is lower than the temperature of the HTS medium 21 entering the hot side CFX 2 at position 32 from a first hot side thermal storage tank 6 at a temperature T₁ ⁺ (i.e., T₀ ⁺<T₁′). As these two fluids pass in thermal contact with each other in the heat exchanger, the working fluid's temperature increases as it moves from position 31 position 34, absorbing heat Q₁ from the HTS medium, while the temperature of the HTS medium in turn decreases as it moves from position 32 to position 33, giving off heat Q₁ to the working fluid. In an example, the working fluid exits the hot side CFX 2 at position 34 at the temperature T₁ ⁺ and the HTS medium exits the hot side CFX 2 at position 33 into the second hot side thermal storage tank 7 at the temperature T₀ ⁺. The heat exchange process can take place at a constant or near-constant pressure such that the working fluid exits the hot side CFX 2 at position 34 at a higher temperature but same pressure P₁, as indicated by P and T↑ at position 34. Similarly, the temperature of the HTS medium 21 decreases in the hot side CFX 2, while its pressure can remain constant or near-constant.

Upon exiting the hot side CFX 2 at position 34 (e.g., at T₁ ⁺, P₁), the working fluid 20 undergoes expansion in the turbine 3 before exiting the turbine at position 35. During the expansion, the pressure and temperature of the working fluid decrease (e.g., to T₁, P₂), as indicated by P↓ and T↓ at position 35. The magnitude of work W₂ generated by the turbine depends on the enthalpy of the working fluid entering the turbine and the degree of expansion. In the discharge mode, heat is added to the working fluid between positions 31 and 34 (in the hot side CFX 2) and the working fluid is expanded back to the pressure at which it initially entered the compressor at position 30 (e.g., P₂). The compression ratio (e.g., P₁/P₂) in the compressor 1 being equal to the expansion ratio in the turbine 3, and the enthalpy of the gas entering the turbine being higher than the enthalpy of the gas exiting the compressor, the work W₂ generated by the turbine 3 is greater than the work W₁ consumed by the compressor 1 (i.e., W₂>W₁).

Because heat was added to the working fluid in the hot side CFX 2, the temperature T₁ at which the working fluid exits the turbine at position 35 is higher than the temperature T₀ at which the working fluid initially entered the compressor at position 30. To close the cycle (i.e., to return the pressure and temperature of the working fluid to their initial values T₀, P₂ at position 30), heat Q₂ is rejected by the working fluid to the CTS medium 22 in the cold side CFX 4 between positions 35 and 30 (i.e., between the turbine 3 and the compressor 1). The CTS medium 22 enters the cold side CFX 4 at position 36 from a second cold side thermal storage tank 9 at the temperature T₀ and exits the cold side CFX 4 at position 37 into a first cold side thermal storage tank 8 at the temperature T₁, while the working fluid 20 enters the cold side CFX 4 at position 35 at the temperature T₁ and exits the cold side CFX 4 at position 30 at the temperature T₀. Again, the heat exchange process can take place at a constant or near-constant pressure such that the working fluid exits the cold side CFX 2 at position 30 at a higher temperature but same pressure P₂, as indicated by P and T↓ at position 30. Similarly, the temperature of the CTS medium 22 increases in the cold side CFX 2, while its pressure can remain constant or near-constant.

During discharge, the heat Q₂ is added to the CTS medium and the heat Q₁ is removed from the HTS medium, wherein Q₁>Q₂. A net amount of work W₂−W₁ is generated, since the work W₁ used by the compressor is smaller than the work W₂ generated by the turbine. A device that generates work while moving heat from a hot body or thermal storage medium to a cold body or thermal storage medium is a heat engine; thus, the pumped thermal system in the discharge mode operates as a heat engine.

FIG. 6 is a simplified schematic perspective view of a closed working fluid system in the pumped thermal system in FIGS. 2-3. As indicated, the working fluid 20 (contained inside tubing) circulates clockwise between the compressor 1, the hot side heat exchanger 2, the turbine 3, and the cold side heat exchanger 4. The compressor 1 and the turbine 3 can be ganged on a common mechanical shaft 10 such that they rotate together. In some implementations, the compressor 1 and the turbine 3 can have separate mechanical shafts. A motor/generator 11 (e.g., including a synchronous motor-synchronous generator converter on a single common shaft) provides power to and from the turbomachinery. In this example, the compressor, the turbine and the motor/generator are all located on a common shaft. Pipes at positions 32 and 33 transfer hot side thermal storage fluid to and from the hot side heat exchanger 2, respectively. Pipes at positions 36 and 37 transfer cold side thermal storage fluid to and from the cold side heat exchanger 4, respectively.

Although the system of FIG. 6 is illustrated as comprising a compressor 1 and turbine 3, the system can include one or more compressors and one or more turbines, which may operate, for example, in a parallel configuration, or alternatively in a series configuration or in a combination of parallel and series configurations. In some examples, a system of compressors or turbines may be assembled such that a given compression ratio is achieved. In some cases, different compression ratios (e.g., on charge and discharge) can be used (e.g., by connecting or disconnecting, in a parallel and/or series configuration, one or more compressors or turbines from the system of compressors or turbines). In some examples, the working fluid is directed to a plurality of compressors and/or a plurality of turbines. In some examples, the compressor and/or turbine may have temperature dependent compression ratios. Arrangement and/or operation of the turbomachinery and/or other elements of the system may be adjusted in accordance with the temperature dependence (e.g., to optimize performance).

FIG. 7 is a simplified schematic perspective view of the pumped thermal system in FIGS. 2-3 with hot side and cold side storage tanks and a closed cycle working fluid system. In this example, the HTS medium is a molten salt and the CTS medium is a low temperature liquid. One, two or more first hot side tanks 6 (at the temperature T₁ ⁺) and one, two or more second hot side tanks 7 (at the temperature T₀ ⁺), both for holding the HTS medium, are in fluid communication with a valve 13 configured to transfer the HTS medium to and from the hot side heat exchanger 2. One, two or more first cold side tanks 8 (at the temperature T₁) and one, two or more second cold side tanks 9 (at the temperature T₀), both for holding the CTS medium, are in fluid communication with a valve 12 configured to transfer the CTS medium to and from the cold side heat exchanger 4.

The thermal energy reservoirs or storage tanks may be thermally insulated tanks that can hold a suitable quantity of the relevant thermal storage medium (e.g., heat storage fluid). The storage tanks may allow for relatively compact storage of large amounts of thermal energy. In an example, the hot side tanks 6 and/or 7 can have a diameter of about 80 meters, while the cold side tanks 8 and/or 9 can have a diameter of about 60 meters. In another example, the size of each (i.e., hot side or cold side) thermal storage for a 1 GW plant operating for 12 hours can be about 20 medium-sized oil refinery tanks.

In some implementations, a third set of tanks containing storage media at intermediate temperatures between the other tanks may be included on the hot side and/or the cold side. In an example, a third storage or transfer tank (or set of tanks) at a temperature intermediate to the temperatures of a first tank (or set of tanks) and a second tank (or set of tanks) may be provided. A set of valves may be provided for switching the storage media between the different tanks and heat exchangers. For example, thermal media may be directed to different sets of tanks after exiting the heat exchangers depending on operating conditions and/or cycle being used. In some implementations, one or more additional sets of storage tanks at different temperatures may be added on the hot side and/or the cold side.

The storage tanks (e.g., hot side tanks comprising hot side thermal storage medium and/or cold side tanks comprising cold side thermal storage medium) may operate at ambient pressure. In some implementations, thermal energy storage at ambient pressure can provide safety benefits. Alternatively, the storage tanks may operate at elevated pressures, such as, for example, at a pressure of at least about 2 atm, at least about 5 atm, at least about 10 atm, at least about 20 atm, or more. Alternatively, the storage tanks may operate at reduced pressures, such as, for example, at a pressure of at most about 0.9 atm, at most about 0.7 atm, at most about 0.5 atm, at most about 0.3 atm, at most about 0.1 atm, at most about 0.01 atm, at most about 0.001 atm, or less. In some cases (e.g., when operating at higher/elevated or lower pressures or to avoid contamination of the thermal storage media), the storage tanks can be sealed from the surrounding atmosphere. Alternatively, in some cases, the storage tanks may not be sealed. In some implementations, the tanks may include one or more pressure regulation or relief systems (e.g., a valve for safety or system optimization).

As used herein, the first hot side tank(s) 6 (at the temperature T₁ ⁺) can contain HTS medium at a higher temperature than the second hot side tank(s) 7 (at the temperature T₀ ⁺), and the first cold side tank(s) 8 (at the temperature T₁) can contain CTS medium at a higher temperature than the second cold side tank(s) 9 (at the temperature T₀). During charge, HTS medium in the first (higher temperature) hot side tank(s) 6 and/or CTS medium in the second (lower temperature) cold side tank(s) 9 can be replenished. During discharge, HTS medium in the first (higher temperature) hot side tank(s) 6 and/or CTS medium in the second (lower temperature) cold side tank(s) 9 can be consumed.

In the foregoing examples, in either mode of operation, two of the four storage tanks 6, 7, 8 and 9 are feeding thermal storage medium to the heat exchangers 2 and 4 at the inlets 32 and 36, respectively, and the other two tanks are receiving thermal storage medium from the heat exchangers 2 and 4 from the exits 33 and 37, respectively. In this configuration, the feed tanks can contain a storage medium at a given temperature due to prior operating conditions, while the receiving tanks' temperatures can depend on current system operation (e.g., operating parameters, loads and/or power input). The receiving tank temperatures may be set by the Brayton cycle conditions. In some cases, the receiving tank temperatures may deviate from desired values due to deviations from predetermined cycle conditions (e.g., variation of absolute pressure in response to system demand) and/or due to entropy generation within the system. In some cases (e.g., due to entropy generation), at least one of the four tank temperatures can be higher than desired. In some implementations, a radiator can be used to reject or dissipate this waste heat to the environment. In some cases, heat rejection to the environment may be enhanced (e.g., using evaporative cooling etc.). The waste heat generated during operation of the pumped thermal systems herein can also be utilized for other purposes. For example, waste heat from one part of the system may be used elsewhere in the system. In another example, waste heat may be provided to an external process or system, such as, for example, a manufacturing process requiring low grade heat, commercial or residential heating, thermal desalination, commercial drying operations etc.

Components of pumped thermal systems of the disclosure may exhibit non-ideal performance, leading to losses and/or inefficiencies. The major losses in the system may occur due to inefficiencies of the turbomachinery (e.g., compressor and turbine) and the heat exchangers. The losses due to the heat exchangers may be small compared to the losses due to the turbomachinery. In some implementations, the losses due to the heat exchangers can be reduced to near zero with suitable design and expense. Therefore, in some analytical examples, losses due to the heat exchangers and other possible small losses due to pumps, the motor/generator and/or other factors may be neglected.

Losses due to turbomachinery can be quantified in terms of adiabatic efficiencies η_(c) and η_(t) (also known as isentropic efficiencies) for compressors and turbines, respectively. For large turbomachinery, typical values may range between η_(c)=0.85-0.9 for compressors and η_(t)=0.9-0.95 for turbines. The actual amount of work produced or consumed by a cycle can then be expressed as

${{\Delta \; W} = {{W_{actual}^{({out})} - W_{actual}^{({in})}} = {{\eta_{t}W_{ideal}^{({out})}} - {\frac{1}{\eta_{c}}W_{ideal}^{({in})}}}}},$

where, in an example assuming constant specific heats of the working fluid, W_(ideal) ^((in))=c_(p)T_(inlet)(ψ−1), W_(ideal) ^((out))=c_(p)T_(inlet)(1−ψ⁻¹), where

${\psi = r^{\frac{\gamma - 1}{\gamma}}},$

r is the compression ratio (i.e., ratio of the higher pressure to the lower pressure), and γ=c_(p)/c_(ν) is the ratio of specific heats of the working fluid. Due to compressor and turbine inefficiencies, more work is required to achieve a given compression ratio during compression, and less work is generated during expansion for a given compression ratio. Losses can also be quantified in terms of the polytropic, or single stage, efficiencies, η_(cp) and η_(tp), for compressors and turbines, respectively. The polytropic efficiencies are related to the adiabatic efficiencies η_(c) and η_(t) by the equations

$\eta_{c} = {{\frac{\psi - 1}{\psi^{1/\eta_{cp}} - 1}\mspace{14mu} {and}\mspace{14mu} \eta_{t}} = {\frac{1 - \psi^{- \eta_{tp}}}{1 - \psi^{- 1}}.}}$

In examples where η_(c)=η_(t)=1, pumped thermal cycles of the disclosure can follow identical paths in both charge and discharge cycles (e.g., as shown in FIGS. 4 and 5). In examples where η_(c)<1 and/or η_(t)<1, compression in the compressor can lead to a greater temperature increase than in the ideal case for the same compression ratio, and expansion in the turbine can lead to a smaller temperature decrease than in the ideal case.

In some implementations, the polytropic efficiency of the compressor η_(cp) may be at least about 0.3, at least about 0.5, at least about 0.6, at least about 0.7, at least about 0.75, at least about 0.8, at least about 0.85, at least about 0.9, at least about 0.91, at least about 0.92, at least about 0.93, at least about 0.96, or more. In some implementations, the polytropic efficiency of the compressor η_(tp) may be at least about 0.3, at least about 0.5, at least about 0.6, at least about 0.7, at least about 0.75, at least about 0.8, at least about 0.85, at least about 0.9, at least about 0.91, at least about 0.92, at least about 0.93, at least about 0.96, at least about 0.97 or more.

T₀ ⁺, T₁ ⁺ were previously defined as the temperatures achieved at the exit of a compressor with a given compression ratio r, adiabatic efficiency η_(c) and inlet temperatures of T₀, T₁ respectively. In some examples, these four temperatures are related by the equation

$\frac{T_{0}^{+}}{T_{0}} = {\frac{T_{1}^{+}}{T_{1}} = {\psi^{1/\eta_{cp}}.}}$

FIG. 8 shows an exemplary heat storage charge cycle for a water (CTS)/molten salt (HTS) system with η_(c)=0.9 and η_(t)=0.95. The dashed lines correspond to η_(c)=η_(t)=1 and the solid lines show the charge cycle with η_(t)=0.95 and η_(c)=0.9. In this example, the CTS medium on the cold side is water, and the HTS medium on the hot side is molten salt. In some cases, the system can include 4 heat storage tanks. In the charge cycle, the working fluid at T₀ and P₂ can exchange heat with a CTS medium in the cold side heat exchanger 4, whereby its temperature can increase to T₁ (assuming negligible pressure drop, its pressure can remain P₂). In the compressor 1 with η_(c)=0.9, the temperature and pressure of the working fluid can increase from T₁, P₂ to T₁ ⁺, P₁. The working fluid can then exchange heat with an HTS medium in the hot side heat exchanger 2, such that its temperature can decrease (at constant pressure P₁, assuming negligible pressure drop). If the working fluid enters the turbine 3 with η_(t)=0.95 at the temperature T₀ ⁺ and expands back to its original pressure P₂, its temperature when exiting the turbine may not be T₀. Instead, the working fluid may enter the turbine at a temperature {tilde over (T)}₀ ⁺ and exit the turbine at the temperature T₀ and pressure P₂. In some examples, the temperatures are related by the relation

$\frac{{\overset{\sim}{T}}_{0}^{+}}{T_{0}} = {\psi^{\eta_{tp}}.}$

In some examples, {tilde over (T)}₀ ⁺ is the temperature at which the working fluid enters the inlet of a turbine with adiabatic efficiency η_(t) and compression ratio r in order to exit at the temperature T₀.

In some implementations, the temperature {tilde over (T)}₀ ⁺ may be incorporated into charge cycles of the disclosure by first heat exchanging the working fluid with the HTS medium from T₁ ⁺ to T₀ ⁺, followed by further cooling the working fluid from T₀ ⁺ to {tilde over (T)}₀ ⁺, as illustrated by section 38 of the cycle in FIG. 8.

FIG. 9 shows an exemplary heat storage discharge (extraction) cycle for the water/molten salt system in FIG. 8 with η_(c)=0.9 and η_(t)=0.95. The dashed lines correspond to η_(c)=η_(t)=1 and the solid lines show the charge cycle with η_(t)=0.95 and η_(c)=0.9. In the discharge cycle, the working fluid at T₁ and P₂ can exchange heat with a CTS medium in the cold side heat exchanger 4, whereby its temperature can decrease to T₀ (assuming negligible pressure drop, its pressure can remain P₂). In the compressor 1 with η_(c)=0.9, the temperature and pressure of the working fluid can increase from T₀, P₂ to T₀ ⁺, P₁. The working fluid can then exchange heat with an HTS medium in the hot side heat exchanger 2, such that its temperature can increase (at constant pressure P₁, assuming negligible pressure drop). Working fluid entering the turbine 3 at T₁ ⁺ may not exit the turbine at the temperature T₁ as in the charge cycle, but may instead exit at a temperature {tilde over (T)}₁, where, in some examples, {tilde over (T)}₁=T₁ ⁺ψ^(−η) ^(tp) . In some examples, {tilde over (T)}₁ is the temperature at which the working fluid exits the outlet of a turbine with adiabatic efficiency η_(t) and compression ratio r after entering the inlet of the turbine at the temperature T₁ ⁺.

In some implementations, the temperature {tilde over (T)}₁ may be incorporated into the discharge cycles of the disclosure by first cooling the working fluid exiting the turbine at {tilde over (T)}₁ to T₁, as illustrated by section 39 of the cycle in FIG. 9, followed by heat exchanging the working fluid with the CTS medium from T₁ to T₀.

The charge and discharge cycles may be closed by additional heat rejection operations in sections 38 (between T₀ ⁺ and {tilde over (T)}₀ ⁺) and 39 (between {tilde over (T)}₁ and T₁), respectively. In some cases, closing the cycles through heat rejection in sections of the cycles where the working fluid can reject heat to ambient at low cost may eliminate the need for additional heat input into the system. The sections of the cycles where the working fluid can reject heat to ambient may be limited to sections where the temperature of the working fluid is high enough above ambient temperature for ambient cooling to be feasible. In some examples, heat may be rejected to the environment in sections 38 and/or 39. For example, heat may be rejected using one or more working fluid to air radiators, intermediate water cooling, or a number of other methods. In some cases, heat rejected in sections 38 and/or 39 may be used for another useful purpose, such as, for example, cogeneration, thermal desalination and/or other examples described herein.

In some implementations, the cycles may be closed by varying the compression ratios between the charge and discharge cycles, as shown, for example, in FIG. 10. The ability to vary compression ratio on charge and discharge may be implemented, for example, by varying the rotation speed of the compressor and/or turbine, by variable stator pressure control, by bypassing a subset of the compression or expansion stages on charge or discharge by the use of valves, or by using dedicated compressor/turbine pairs for charge and discharge mode. In one example, the compression ratio in the discharge cycle in FIG. 9 can be changed such that heat rejection in section is 39 is not used, and only heat rejection in section 38 in the charge cycle is used. Varying the compression ratio may allow heat (i.e., entropy) to be rejected at a lower temperature, thereby increasing overall roundtrip efficiency. In some examples of this configuration, the compression ratio on charge, r_(C), can be set such that

${\frac{T_{1}^{+}}{T_{1}} = \psi_{C}^{1/\eta_{cp}}},$

and on discharge, the compression ratio r_(D) can be set such that

$\frac{T_{1}^{+}}{T_{1}} = {\psi_{D}^{\eta_{tp}}.}$

In some cases, the upper temperatures T₁ ⁺ and T₁ can be identical on charge and discharge and no heat removal may be needed in this portion (also “leg” herein) of the cycle. In such cases, the temperature T₀ ⁺ on charge (e.g., T₀ ^(+(c))=T₀ψ_(C) ^(η) ^(tp) ) and the temperature T₀ ⁺ on discharge (e.g., T₀ ^(+(d))=T₀ψ_(D) ^(1/η) ^(cp) ) can be dissimilar and heat may be rejected (also “dissipated” or “dumped” herein) to the environment between the temperatures T₀ ^(+(c)) and T₀ ^(+(d)). In an implementation where only the storage media exchange heat with the environment, a heat rejection device (e.g., devices 55 and 56 shown in FIG. 16) can be used to lower the temperature of the CTS from T₀ ^(+(d)) to T₀ ^(+(c)) between discharge and charge.

FIG. 10 shows an example of a cycle with variable compression ratios. The compression ratio can be higher on discharge (when work is produced by the system) than on charge (when work is consumed by the system), which may increase an overall round trip efficiency of the system. For example, during a charge cycle 80 with T₀ ^(+(c)), a lower compression ratio of <3 can be used; during a discharge cycle 81 with T₀ ^(+(d)), a compression ratio of >3 can be used. The upper temperatures reached in both cycles 80 and 81 can be T₁ and T₁ ⁺, and no excess heat may be rejected.

The compression ratio may be varied between charge and discharge such that the heat dissipation to the environment needed for closing the cycle on both charge and discharge occurs between the temperatures T₀ ^(+(C)) (the temperature of the working fluid before it enters the turbine during the charge cycle) and T₀ ^(+(D)) (the temperature of the working fluid as it exits the compressor on discharge) and not above the temperature T₁ (the temperature of the working fluid before it enters the compressor on charge and/or exits the turbine on discharge). In some examples, none of the heat is rejected at a temperature above the lowest temperature of the HTS medium.

In the absence of system losses and/or inefficiencies, such as, for example, in the case of pumped thermal systems comprising heat pump(s) and heat engine(s) operating at the zero entropy creation/isentropic limit, a given amount of heat Q_(H) can be transferred using a given quantity of work W in heat pump (charge) mode, and the same Q_(H) can be used in heat engine (discharge) mode to produce the same work W, leading to a unity (i.e., 100%) roundtrip efficiency. In the presence of system losses and/or inefficiencies, roundtrip efficiencies of pumped thermal systems may be limited by how much the components deviate from ideal performance.

The roundtrip efficiency of a pumped thermal system may be defined as η_(store)=|W_(cv) ^(extract)|/|W_(cv) ^(charge)|. In some examples, with an approximation of ideal heat exchange, the roundtrip efficiency can be derived by considering the net work output during the discharge cycle,

${{W_{cv}^{extract}} = {{\eta_{t}W_{ideal}^{out}} - \frac{W_{ideal}^{i\; n}}{\eta_{c}}}},$

and the net work input during the charge cycle,

${W_{cv}^{charge}} = {\frac{W_{ideal}^{i\; n}}{\eta_{c}} - {\eta_{t}W_{ideal}^{out}}}$

using the equations for work and temperature given above.

Roundtrip efficiencies may be calculated for different configurations of pumped thermal systems (e.g., for different classes of thermal storage media) based on turbomachinery component efficiencies, η_(c) and η_(t).

In one example, FIG. 11 shows roundtrip efficiency contours for a water/salt system, such as, for example, the water/salt system in FIGS. 8 and 9 with T₀=273 K (0° C.), T₁=373 K (100° C.) and a compression ratio of r=5.65 chosen to achieve compatibility with the salt(s) on the hot side. Exemplary roundtrip efficiency contours at values of η_(store) of 10%, 20%, 30%, 40%, 50%, 60%, 70%, 80% and 90% are shown as a function of component efficiencies η_(c) and η_(t) on the x- and y-axes, respectively. The symbols ⊕ and ⊗ represent the approximate range of present large turbomachinery adiabatic efficiency values. The dashed arrows represent the direction of increasing efficiency.

FIG. 12 shows roundtrip efficiency contours for a colder storage/salt system, such as, for example a hexane/salt system with a gas-gas heat exchanger in FIGS. 13, 14, 17 and 18 with T₀=194 K (−79° C.), T₁=494 K (221° C.) and a compression ratio of r=3.28. Exemplary roundtrip efficiency contours at values of η_(store) of 10%, 20%, 30%, 40%, 50%, 60%, 70%, 80% and 90% are shown as a function of component efficiencies η_(c) and η_(t) on the x- and y-axes, respectively. The symbols ⊕ and ⊗ represent the approximate range of present large turbomachinery adiabatic efficiency values. As discussed in detail elsewhere herein, using hexane, heptane and/or another CTS medium capable of low temperature operation may result in significant improvements of system efficiency.

Pumped Thermal Storage Cycles with Recuperation

Another aspect of the disclosure is directed to pumped thermal systems with recuperation. In some situations, the terms regeneration and recuperation can be used interchangeably, although they may have different meanings. As used herein, the terms “recuperation” and “recuperator” generally refer to the presence of one or more additional heat exchangers where the working fluid exchanges heat with itself during different segments of a thermodynamic cycle through continuous heat exchange without intermediate thermal storage. The roundtrip efficiency of pumped thermal systems may be substantially improved if the allowable temperature ranges of the storage materials can be extended. In some implementations, this may be accomplished by choosing a material or medium on the cold side that can go to temperatures below 273 K (0° C.). For example, a CTS medium (e.g., hexane) with a low temperature limit of approximately T₀=179 K (−94° C.) may be used in a system with a molten salt HTS medium. However, T₀ ⁺ (i.e., the lowest temperature of the working fluid in the hot side heat exchanger) at some (e.g., modest) compression ratios may be below the freezing point of the molten salt, making the molten salt unviable as the HTS medium. In some implementations, this can be resolved by including a working fluid to working fluid (e.g., gas-gas) heat exchanger (also “recuperator” herein) in the cycle.

FIG. 13 is a schematic flow diagram of working fluid and heat storage media of a pumped thermal system in a charge/heat pump mode with a gas-gas heat exchanger 5 for the working fluid. The use of the gas-gas heat exchanger can enable use of colder heat storage medium on the cold side of the system. The working fluid can be air. The working fluid can be dry air. The working fluid can be nitrogen. The working fluid can be argon. The working fluid can be a mixture of primarily argon mixed with another gas such as helium. For example, the working fluid may comprise at least about 50% argon, at least about 60% argon, at least about 70% argon, at least about 80% argon, at least about 90% argon, or about 100% argon, with balance helium.

FIG. 17 shows a heat storage charge cycle for the storage system in FIG. 13 with a cold side storage medium (e.g., liquid hexane) capable of going down to approximately to 179 K (−94° C.) and a molten salt as the hot side storage, and η_(c)=0.9 and η_(t)=0.95. The CTS medium can be hexane or heptane and the HTS medium can be molten salt. In some cases, the system can include four heat storage tanks.

In one implementation, during charge in FIGS. 13 and 17, the working fluid enters the compressor at T₁ and P₂, exits the compressor at T₁ ⁺ and P₁, rejects heat Q₁ to the HTS medium 21 in the hot side CFX 2, exiting the hot side CFX 2 at T₁ and P₁, rejects heat Q_(recup) (also “Q_(regen)” herein, as shown, for example, in the accompanying drawings) to the cold (low pressure) side working fluid in the heat exchanger or recuperator 5, exits the recuperator 5 at T₀ ⁺ and P₁, rejects heat to the environment (or other heat sink) in section 38 (e.g., a radiator), enters the turbine 3 at {tilde over (T)}₀ ⁺ and P₁, exits the turbine at T₀ and P₂, absorbs heat Q₂ from the CTS medium 22 in the cold side CFX 4, exiting the cold side CFX 4 at T₀ ⁺ and P₂, absorbs heat Q_(recup) from the hot (high pressure) side working fluid in the heat exchanger or recuperator 5, and finally exits the recuperator 5 at T₁ and P₂, returning to its initial state before entering the compressor.

FIG. 14 is a schematic flow diagram of working fluid and heat storage media of the pumped thermal system in FIG. 13 in a discharge/heat engine mode. Again, the use of the gas-gas heat exchanger can enable use of colder heat storage fluid (CTS) and/or colder working fluid on the cold side of the system.

FIG. 18 shows a heat storage discharge cycle for the storage system for the storage system in FIG. 14 with a cold side storage medium (e.g., liquid hexane) capable of going down to 179 K (−94° C.) and a molten salt as the hot side storage, and η_(c)=0.9 and η_(t)=0.95. Again, the CTS medium can be hexane or heptane and the HTS medium can be molten salt, and the system may include 4 heat storage tanks.

During discharge in FIGS. 14 and 18, the working fluid enters the compressor at T₀ and P₂, exits the compressor at T₀ ⁺ and P₁, absorbs heat Q_(recup) from the cold (low pressure) side working fluid in the heat exchanger or recuperator 5, exits the recuperator 5 at T₁ and P₁, absorbs heat Q₁ from the HTS medium 21 in the hot side CFX 2, exiting the hot side CFX 2 at T₁ ⁺ and P₁, enters the turbine 3 at T₁ ⁺ and P₁, exits the turbine at {tilde over (T)}₁ and P₂, rejects heat to the environment (or other heat sink) in section 39 (e.g., a radiator), rejects heat Q_(recup) to the hot (high pressure) side working fluid in the heat exchanger or recuperator 5, enters the cold side CFX 4 at T₀ ⁺ and P₂, rejects heat Q₂ to the CTS medium 22 in the cold side CFX 4, and finally exits the cold side CFX 4 at T₀ and P₂, returning to its initial state before entering the compressor.

In another implementation, shown in FIG. 15, the charge cycle remains the same as in FIGS. 13 and 17, except that the working fluid exits the recuperator 5 at {tilde over (T)}₀ ⁺ and P₁ (instead of at T₀ ⁺ and P₁ as in FIGS. 13 and 17), enters the turbine 3 at {tilde over (T)}₀ ⁺ and P₁, exits the turbine at T₀ and P₂, absorbs heat Q₂ from the CTS medium 22 having a temperature {tilde over (T)}₀ ⁺ (instead of at T₀ ⁺ as in FIGS. 13 and 17) in the cold side CFX 4, and exits the cold side CFX 4 at {tilde over (T)}₀ ⁺ and P₂ (instead of at T₀ ⁺ and P₂ as in FIG. 13) before reentering the recuperator 5. The heat between temperatures T₀ ⁺ and {tilde over (T)}₀ ⁺ is no longer rejected from the working fluid to the environment directly (as in section 38 in FIGS. 13 and 17).

During discharge in FIG. 16, the discharge cycle remains the same as in FIGS. 14 and 8B, except that the temperature of the HTS medium being deposited in tank 7 is changed. The working fluid exits the recuperator 5 at {tilde over (T)}₁ and P₁ (instead of at T₁ and P₁ as in FIGS. 14 and 8B) and absorbs heat Q₁ from the HTS medium 21 in the hot side CFX 2. The HTS medium exits the hot side CFX 2 having a temperature {tilde over (T)}₁ (instead of at T₁ as in FIGS. 14 and 18). The working fluid then exits the hot side CFX 2 at T₁ ⁺ and P₁, enters the turbine 3 at T₁ ⁺ and P₁, and exits the turbine at {tilde over (T)}₁ and P₂ before reentering the recuperator 5. The heat between temperatures {tilde over (T)}₁ and T₁ is no longer rejected from the working fluid to the environment directly (as in section 39 in FIGS. 14 and 18). As in FIG. 14, the CTS medium enters the tank 8 at temperature T₀ ⁺.

After the discharge in FIG. 16, in preparation for the charge in FIG. 15, heat exchange with ambient may be used to cool the HTS medium 21 from the temperature {tilde over (T)}₁ used in the discharge cycle to the temperature T₁ used in the charge cycle. Similarly, heat exchange with ambient may be used to cool the CTS medium 22 from the temperature T₀ ⁺ used in the discharge cycle to the temperature {tilde over (T)}₀ ⁺ used in the charge cycle. Unlike in the configuration in FIGS. 13 and 14, where the working fluid may need to reject a substantial amount of heat (in sections 38 and 39, respectively) at a fast rate, in this configuration, the hot side and cold side storage media may be cooled at an arbitrarily slow rate (e.g., by radiating away or by other means of giving off the heat to the environment).

As shown in FIG. 16, in some implementations, heat can be rejected from the CTS medium to the environment by circulating the CTS medium in the tank 8 in a heat rejection device 55 that can absorb heat from the CTS medium and reject heat to the environment until the CTS medium cools from the temperature T₀ ⁺ to the temperature {tilde over (T)}₀ ⁺. In some examples, the heat rejection device 55 can be, for example, a radiator, a thermal bath containing a substance such as water or salt water, or a device immersed in a natural body of water such as a lake, river or ocean. In some examples, the heat rejection device 55 can also be an air cooling apparatus, or a series of pipes which are thermally connected to a solid reservoir (e.g., pipes embedded in the ground).

Similarly, in some implementations, heat can be rejected from the HTS medium to the environment by circulating the HTS in the tank 7 in a heat rejection device 56 that can absorb heat from the HTS medium and reject heat to the environment until the HTS medium cools from the temperature {tilde over (T)}₁ to the temperature T₁. In some examples, the heat rejection device 56 can be, for example, a radiator, a thermal bath containing a substance such as water or salt water, or a device immersed in a natural body of water such as a lake, river or ocean. In some examples, the heat rejection device 56 can also be an air cooling apparatus or a series of pipes which are thermally connected to a solid reservoir (e.g., pipes embedded in the ground).

In some implementations, rejecting heat to ambient through the use of the thermal storage media may be used in conjunction with the variable compression ratio charge and/or discharge cycles described, for example, in FIG. 10. In this system, only the CTS medium may exchange heat with ambient. Such a system can also be implemented with a recuperator to extend the temperature ranges of the HTS and CTS media in the cycles.

In some implementations, three separate cold side storage tanks at respective temperatures T₀, {tilde over (T)}₀ ⁺ and T₀ ⁺ may be used (e.g., an extra tank may be used in addition to the tanks 8 and 9). During heat exchange in the cold side CFX 4 in the discharge cycle, heat from the working fluid exiting the recuperator 5 may be transferred to the CTS medium in the T₀ ⁺-tank. The CTS medium may be cooled in/by, for example, the heat rejection device 55 prior to entering the {tilde over (T)}₀ ⁺-tank. In some implementations, three separate hot side storage tanks at respective temperatures T₁, {tilde over (T)}₁ and T₁ ⁺ may be used (e.g., an extra tank may be used in addition to the tanks 6 and 7). During heat exchange in the hot side CFX 2 in the discharge cycle, heat from the working fluid exiting the recuperator 5 may be transferred to the HTS medium in the {tilde over (T)}₁-tank. The HTS medium may be cooled in/by, for example, the heat rejection device 56 prior to entering the T₁-tank. Heat rejection to the environment in such a manner may present several advantages. In a first example, it may eliminate the need for a potentially expensive working fluid to ambient heat exchanger that is capable of absorbing heat from the working fluid at a rate proportional to the power input/output of the system. The HTS and CTS media may instead reject heat over extended time periods, thus reducing the cost of the cooling infrastructure. In a second example, it may allow the decision regarding when heat is rejected to the environment to be delayed such that heat exchange to ambient may be performed when temperature (e.g., the ambient temperature) is most favorable.

In the charge and discharge cycles of FIGS. 13 and 17, and FIGS. 14 and 18, respectively, the same compression ratios and temperature values are used for both charge and discharge. In this configuration, the roundtrip efficiency can be about η_(store)=74%, as given by T₀=194 K (−79° C.), T₁=494 K (221° C.). η_(t)=0.95, η_(c)=0.9 and r=3.3.

Thus, in some examples involving working fluid to working fluid recuperation, heat rejection on the hot side (high pressure) side of the closed charge cycle can take place in three operations (heat exchange with the HTS medium, followed by recuperation, followed by heat rejection to the environment), and heat rejection on the cold side (low pressure) side of the closed discharge cycle can take place in three operations (heat rejection to the environment, followed by recuperation, followed by heat exchange with the CTS medium). As a result of recuperation, the higher temperature HTS tank(s) 6 can remain at T₁ ⁺ while the lower temperature HTS tank(s) 7 can now be at the temperature T₁>T₀ ⁺, and the lower temperature CTS tank(s) 9 can remain at T₀ while the higher temperature CTS tank(s) 8 can now be at the temperature T₀ ⁺<T₁.

In some cases, recuperation may be implemented using the heat exchanger 5 for direct transfer of heat between the working fluid on the high pressure side and the working fluid on the low pressure side. In an alternative configuration, an additional pair (or plurality) of heat exchangers together with an additional heat transfer medium or fluid (e.g., a dedicated thermal heat transfer fluid that is liquid in an appropriate temperature range, such as, for example, Therminol®) may be used to achieve recuperation. For example, an additional heat exchanger may be added in series with the cold side heat exchanger and an additional heat exchanger may be added in series with the hot side heat exchanger. The additional heat transfer medium may circulate between the two additional heat exchangers in a closed loop. In other examples, one or more additional heat exchangers may be placed elsewhere in the system to facilitate recuperation. Further, one or more additional heat transfer media or mixtures thereof may be used. The one or more additional heat transfer media fluids may be in fluid or thermal communication with one or more other components, such as, for example, a cooling tower or a radiator.

In one example, hexane or heptane can be used as a CTS medium, and nitrate salt can be used as an HTS medium. On the low pressure side of the cycle, the operating temperatures of the pumped thermal storage cycles may be limited by the melting point of hexane (178 K or −95° C.) at T₀ and by the melting point of the nitrate (494 K or 221° C.) at T₁. On the high pressure side of the cycle, the operating temperatures may be limited by the boiling point of hexane (341 K or 68° C.) at T₀ ⁺ and by the decomposition of nitrate (873 K or 600° C.) at T₁ ⁺. At these conditions, the high pressure and low pressure temperature ranges can overlap such that recuperation can be implemented. The actual temperatures T₀, T₁, T₀ ⁺ and T₁ ⁺ and pressure ratios implemented in hexane/nitrate systems may differ from the limits above.

In some examples, recuperation may enable the compression ratio to be reduced. In some cases, reducing the compression ratio may result in reduced compressor and turbine losses. In some cases, the compression ratio may be at least about 1.2, at least about 1.5, at least about 2, at least about 2.5, at least about 3, at least about 3.5, at least about 4, at least about 4.5, at least about 5, at least about 6, at least about 8, at least about 10, at least about 15, at least about 20, at least about 30, or more.

In some cases, T₀ may be at least about 30 K, at least about 50 K, at least about 80 K, at least about 100 K, at least about 120 K, at least about 140 K, at least about 160 K, at least about 180 K, at least about 200 K, at least about 220 K, at least about 240 K, at least about 260 K, or at least about 280 K. In some cases, T₀ ⁺ may be at least about 220 K, at least about 240 K, at least about 260 K, at least about 280 K, at least about 300 K, at least about 320 K, at least about 340 K, at least about 360 K, at least about 380 K, at least about 400 K, or more. In some cases, the temperatures T₀ and T₀ ⁺ can be constrained by the ability to reject excess heat to the environment at ambient temperature. In some cases. the temperatures T₀ and T₀ ⁺ can be constrained by the operating temperatures of the CTS (e.g., a phase transition temperature). In some cases, the temperatures T₀ and T₀ ⁺ can be constrained by the compression ratio being used. Any description of the temperatures T₀ and/or T₀ ⁺ herein may apply to any system or method of the disclosure.

In some cases, T₁ may be at least about 350K, at least about 400 K, at least about 440 K, at least about 480 K, at least about 520 K, at least about 560 K, at least about 600 K, at least about 640 K, at least about 680 K, at least about 720 K, at least about 760 K, at least about 800 K, at least about 840 K, at least about 880 K, at least about 920 K, at least about 960 K, at least about 1000 K, at least about 1100 K, at least about 1200 K, at least about 1300 K, at least about 1400 K, or more. In some cases, T₁ ⁺ may be at least about 480 K, at least about 520 K, at least about 560 K, at least about 600 K, at least about 640 K, at least about 680 K, at least about 720 K, at least about 760 K, at least about 800 K, at least about 840 K, at least about 880 K, at least about 920 K, at least about 960 K, at least about 1000 K, at least about 1100 K, at least about 1200 K, at least about 1300 K, at least about 1400 K, at least about 1500 K, at least about 1600 K, at least about 1700 K, or more. In some cases. the temperatures T₁ and T₁ ⁺ can be constrained by the operating temperatures of the HTS. In some cases. the temperatures T₁ and T₁ ⁺ can be constrained by the thermal limits of the metals and materials being used in the system. For example, a conventional solar salt can have a recommended temperature range of approximately 560-840 K. Various system improvements, such as, for example, increased roundtrip efficiency, increased power and increased storage capacity may be realized as available materials, metallurgy and storage materials improve over time and enable different temperature ranges to be achieved. Any description of the temperatures T₁ and/or T₁ ⁺ herein may apply to any system or method of the disclosure.

In some cases, the roundtrip efficiency η_(store) (e.g., electricity storage efficiency) with and/or without recuperation can be at least about 5%, at least about 10%, at least about 15%, at least about 20%, at least about 25%, at least about 30%, at least about 35%, at least about 40%, at least about 45%, at least about 50%, at least about 55%, at least about 60%, at least about 65%, at least about 70%, at least about 75%, at least about 80%, at least about 85%, at least about 90%, or at least about 95%.

In some implementations, at least a portion of heat transfer in the system (e.g., heat transfer to and from the working fluid) during a charge and/or discharge cycle includes heat transfer with the environment (e.g., heat transfer in sections 38 and 39). The remainder of the heat transfer in the system can occur through thermal communication with thermal storage media (e.g., thermal storage media 21 and 22), through heat transfer in the recuperator 5 and/or through various heat transfer processes within system boundaries (i.e., not with the surrounding environment). In some examples, the environment may refer to gaseous or liquid reservoirs surrounding the system (e.g., air, water), any system or medium capable of exchanging thermal energy with the system (e.g., another thermodynamic cycle or system, heating/cooling systems, etc.), or any combination thereof. In some examples, heat transferred through thermal communication with the heat storage media can be at least about 25%, at least about 50%, at least about 60%, at least about 70%, at least about 80%, or at least about 90% of all heat transferred in the system. In some examples, heat transferred through heat transfer in the recuperator can be at least about 5%, at least about 10%, at least about 15%, at least about 20%, at least about 25%, at least about 50%, or at least about 75% of all heat transferred in the system. In some examples, heat transferred through thermal communication with the heat storage media and through heat transfer in the recuperator can be at least about 25%, at least about 50%, at least about 60%, at least about 70%, at least about 80%, at least about 90%, or even about 100% of all heat transferred in the system. In some examples, heat transferred through heat transfer with the environment can be less than about 5%, less than about 10%, less than about 15%, less than about 20%, less than about 30%, less than about 40%, less than about 50%, less than about 60%, less than about 70%, less than about 80%, less than about 90%, less than about 100%, or even 100% of all heat transferred in the system. In some implementations, all heat transfer in the system may be with the thermal storage media (e.g., the CTS and HTS media), and only the thermal storage media may conduct heat transfer with the environment.

Pumped thermal cycles of the disclosure (e.g., the cycles in FIGS. 13 and 14) may be implemented through various configurations of pipes and valves for transporting the working fluid between the turbomachinery and the heat exchangers. In some implementations, a valving system may be used such that the different cycles of the system can be interchanged while maintaining the same or nearly the same temperature profile across at least one, across a subset or across all of counter-flow heat exchangers in the system. For example, the valving may be configured such that the working fluid can pass through the heat exchangers in opposite flow directions on charge and discharge and flow directions of the HTS and CTS media are reversed by reversing the direction of the pumps.

In some implementations, the system with a recuperator may have a different compression and/or expansion ratio on charge and discharge. This may then involve heat rejection at only one or both of the heat rejection locations 38 and 39 as shown in FIG. 5C along the lines described above.

FIG. 19 is a schematic flow diagram of hot side recharging in a pumped heat cycle in solar mode with heating of a solar salt solely by solar power. The system can comprise a solar heater for heating the hot side heat storage. The HTS medium 21 in the second hot thermal storage tank 7 of a discharge cycle, such as, for example, the HTS medium of the discharge cycle in FIG. 14, can be recharged within element 17 using heating provided by solar radiation. The HTS medium (e.g., molten salt) can be heated by solar heating from the temperature T₁ in the second hot thermal storage tank 7 to the temperature T₁ ⁺ in the first hot thermal storage tank 6.

In some implementations, such as, for example, for the systems in FIG. 19 solar heat for heating the HTS medium (e.g., from T₁=493 K (220° C.) to T₁ ⁺=873 K (600° C.)) may be provided by a concentrating solar facility. In some examples, a small scale concentrating facility may be utilized for providing heat. In some cases, the concentrating solar facility may include one or more components for achieving high solar concentrating efficiency, including, for example, high-performance actuators (e.g., adaptive fluidic actuators manufactured from polymers), mutiplexing control system, dense heliostat layout etc. In some examples, the heat provided for heating the HTS medium (e.g., in the element 17) may be a waste heat stream from the concentrating solar facility.

FIG. 20 is a schematic flow diagram of a pumped thermal system discharge cycle that can be coupled with external heat input (e.g., solar, combustion) with heat rejection to ambient. Such a discharge cycle may be used, for example, in situations where the capacity for hot side recharging (e.g., using solar heating, waste heat or combustion) is greater than the capacity for cold side recharging. Solar heat may be used to charge the HTS medium 21 in the hot side storage tanks from T₁ to T₁ ⁺, as described elsewhere herein. The discharge cycle can operate similarly to the discharge cycle in FIG. 3, but after exiting the turbine 3, the working fluid 20 can proceed to the cold side CFX 4 heat exchanger 4 where it exchanges heat with an intermediate thermal storage (ITS) medium 61 having a lower temperature T₀ at or near ambient temperature. The ITS medium 61 enters the cold side CFX 4 from a second intermediate thermal storage tank 59 at the temperature T₀ (e.g., ambient temperature) and exits the cold side CFX 4 into a first intermediate thermal storage tank 60 at the temperature {tilde over (T)}₁, while the working fluid 20 enters the cold side CFX 4 at the temperature {tilde over (T)}₁ and exits the cold side CFX 4 at the temperature T₀. The working fluid enters the compressor 1 at T₀ and P₂, exits the compressor at T₀ ⁺ and P₁, absorbs heat Q₁ from the HTS medium 21 in the hot side CFX 2, exits the hot side CFX 2 at T₁ ⁺ and P₁, enters the turbine 3 at T₁ ⁺ and P₁, exits the turbine at {tilde over (T)}₁ and P₂, rejects heat Q₂ from the ITS medium 61 in the cold side CFX 4, and exits the cold side CFX 4 at T₀ and P₂, returning to its initial state before entering the compressor.

In some implementations, the ITS medium 61 may be a liquid over the entire range from T₀ to {tilde over (T)}₁. In other implementations, the ITS medium 61 may not be a liquid over the entire range from □₀ to {tilde over (T)}₁, but may be provided to the counter-flow heat exchanger 4 at a higher flow rate in order to achieve a lower temperature rise across the counter-flow heat exchanger (e.g., such that the temperature of the ITS medium at the exit of the counter-flow heat exchanger 4 is lower than {tilde over (T)}₁) while still cooling the working fluid from {tilde over (T)}₁ to T₀. In this instance, the temperature of the ITS medium in the tank 60 can be lower than {tilde over (T)}₁. The ITS medium in the tank 60 can exchange heat with ambient (e.g., through a radiator or other implementations described herein) in order to cool back to the temperature T₀. In some cases, the ITS medium can then be returned to the tank 59. In some cases, the heat deposited in the ITS medium may be used for various useful purposes such as, for example, residential or commercial heating, thermal desalination or other uses described elsewhere herein.

FIG. 21 is a schematic flow diagram of a pumped thermal system discharge cycle in solar mode or combustion heated mode with heat rejection to an intermediate fluid circulated in a thermal bath at ambient temperature. The discharge cycle can operate similarly to the discharge cycle in FIG. 20, but after exiting the turbine 3, the working fluid 20 can proceed to the cold side CFX 4 where it exchanges heat with an intermediate medium or fluid 62 circulating through a thermal bath 63 at the temperature T₀ at or near ambient temperature. The intermediate medium or fluid 62 (e.g., Therminol®, or a heat transfer oil) may be used for exchanging heat between the working fluid 20 and a thermal bath 63 in the cold side CFX 4. The use of the intermediate fluid 62 may provide an advantage over contacting an inexpensive thermal sink or medium (e.g., water) directly with the working fluid. For example, directly contacting such a thermal medium with the working fluid in the cold side CFX 4 may cause problems, such as, for example, evaporation or over-pressurization (e.g., explosion) of the thermal medium. The intermediate fluid 62 can remain in liquid phase throughout all, at least a portion of, or a significant portion of the operation in the cold side CFX 4. As the intermediate fluid 62 passes through the thermal bath 58, it can be sufficiently cooled to circulate back into the cold side CFX 4 for cooling the working fluid from D₁ to T₀. The thermal bath 63 may contain a large amount of inexpensive heat sink material or medium, such as, for example, water. In some cases, the heat deposited in the heat sink material may be used for various useful purposes such as, for example, residential or commercial heating, thermal desalination or other uses described elsewhere herein. In some cases, the heat sink material may be re-equilibrated with ambient temperature (e.g., through a radiator or other implementations described herein).

In some implementations, the discharge cycles in FIGS. 20 and/or 21 may include a recuperator, as described in greater detail in examples throughout the disclosure. Such systems may be implemented using the temperatures T₁ ⁺, T₁, T₀ ⁺ and T₀ described in greater detail elsewhere herein.

Solar Assisted Pumped Thermal Storage Cycles with Intercooling

In some instances, the pumped thermal system may provide heat sources and/or cold sources to other facilities or systems such as, for example, through co-location with a gas to liquids (GTL) facility or a desalination facility. In one example, the GTL facilities may make use of one or more of the cold reservoirs in the system (e.g., the CTS medium in the tank 9 for use in oxygen separation in the GTL facility) and/or one or more hot reservoirs in the system (e.g., the HTS medium in the tank 6 for use in a Fischer-Tropsch process in the GTL facility). In another example, one or more hot reservoirs or one or more cold reservoirs in the pumped thermal system may be used for the operation of thermal desalination methods. Further examples of possible heat and cold uses include co-location or heat exchange with building/area heating and cooling systems.

Conversely, in some cases, the pumped thermal system may make use of waste heat sources and/or waste cold sources from other facilities or systems such as, for example, through co-location with a liquefied natural gas import or export terminal. For example, a waste cold source may be used for cooling the cold side thermal storage media 22. In some implementations, recharging of the cold side using waste cold may be combined with recharging of the hot side thermal storage media 21 by external heat input (e.g., solar, combustion, waste heat, etc.). In some cases, the recharged storage media can then be used in a discharge cycle such as, for example, the discharge cycles in FIG. 14 or 16. In some cases, the pumped thermal system may be used as a heat engine with a waste heat source serving as the hot side heat input and a waste cold source serving as the cold side heat sink. In another implementation, the hot side storage media may be recharged using a modified version of the cycle shown in FIG. 15, where the temperature T₀ is about the ambient temperature and {tilde over (T)}₀ ⁺ corresponds to a temperature above the ambient temperature. In some examples, a waste heat source can be used to provide the heat needed at a temperature of at least {tilde over (T)}₀ ⁺ for heating the working fluid and/or the CTS medium to {tilde over (T)}₀ ⁺. In another implementation, an intermediate fluid (e.g., Therminol®) which can remain liquid between the temperatures {tilde over (T)}₀ ⁺ and T₀ may be used to transfer the heat from the waste heat source to the working fluid.

Pumped Thermal Systems with Dedicated Compressor/Turbine Pairs

In a further aspect of the disclosure, pumped thermal systems comprising multiple working fluid systems, or working fluid flow paths are provided. In some cases, pumped thermal system components in the charge and discharge modes may be the same. For example, the same compressor/turbine pair may be used in charge and discharge cycles. Alternatively, one or more system components may differ between charge and discharge modes. For example, separate compressor/turbine pairs may be used in charge and discharge cycles. In one implementation, the system has one set of heat exchangers, and a common set of HTS and CTS tanks which are charged or discharged by two pairs or sets of compressors and turbines. In another implementation, the system has a common set of HTS and CTS tanks, but separate sets of heat exchangers and separate sets of compressors and turbines.

Pumped thermal systems with recuperation, utilization of external sources of heat, cold and/or waste heat/cold may benefit from having separate compressor/turbine pairs as a result of operation of turbomachinery over large and/or different temperature ranges in charge and discharge modes. For example, temperature changes between charge and discharge cycles may lead to a thermal adjustment period or other difficulties during transition between the cycles (e.g., issues or factor related to metallurgy, thermal expansion, Reynolds number, temperature dependent compression ratios, tip clearance and/or bearing friction etc.). In another example, turbomachinery (e.g., turbomachinery used in systems with recuperation) may operate over a relatively low pressure ratio (e.g., with relatively few compression stages) but over relatively large temperature during both compression and expansion. The temperature ranges may change (e.g., switch as in FIGS. 17 and 18) between charge and discharge modes. In some cases, the operation over large temperature ranges during compression and/or expansion may complicate design of a combined compressor/turbine for both charge and discharge. Furthermore, recuperation, waste heat/cold incorporation and/or other pumped thermal system features may reduce the compression ratio of the compressor/turbine in the charge cycle and/or the discharge cycle, thereby reducing the cost associated with duplicating compressor/turbine sets.

FIGS. 22 and 23 show pumped thermal systems with separate compressor 1/turbine 3 pairs for charge mode C and discharge mode D. The separate compressor/turbine pairs may or may not be ganged on a common mechanical shaft. In this example, the compressor/turbine pairs C and D can have separate shafts 10. The shafts 10 may rotate at the same speed or at different speeds. The separate compressor/turbine pairs or working fluid systems may or may not share heat exchangers (e.g., the heat exchangers 2 and 4).

In the example in FIG. 22, the system has a common set of HTS tanks 6 and 7 and CTS tanks 8 and 9. The system has separate pairs of heat exchangers 2 and 4 and separate compressor 1/turbine 3 pairs for the charge mode C and the discharge mode D. The HTS and CTS storage media flow paths for the charging cycle are shown as solid black lines. The HTS and CTS storage media flow paths for the discharge cycle are shown as the dashed grey lines.

In the example in FIG. 23, the system, shown in a charge configuration, has one set of heat exchangers 2 and 4, and a common set of HTS tanks 6 and 7 and CTS tanks 8 and 9. The HTS and CTS tanks can be charged by a compressor/turbine set C, or discharged by a compressor/turbine set D, each set comprising a compressor 1 and a turbine 3. The system may switch between the sets C and D using valves 83. In the example in FIG. 22, the system, again shown in a charge configuration, has a common set of HTS tanks 6 and 7 and CTS tanks 8 and 9. The HTS and CTS tanks can be charged by the charge set C that includes a first set of the heat exchangers 2 and 4, the compressor 1 and the turbine 3. The HTS and CTS tanks can be discharged by switching to a separate discharge set C that includes a second set of the heat exchangers 2 and 4, the compressor 1 and the turbine 3.

In one example, if the charge and discharge sets of compressors and turbines in FIGS. 22 and 23 are not operated at the same time, the charge and discharge sets may share a common set of heat exchangers that are switched between the turbomachinery pairs using the valves 83. In another example, if the charge and discharge turbomachinery sets or pairs in FIGS. 22 and 23 are operated at the same time (e.g., in order for one set to charge, following intermittent generation, and the other set to discharge at the same time, following load), then each set of turbomachinery may have a dedicated set of heat exchangers. In this instance, the charge and discharge sets may or may not share a set of HTS and CTS tanks.

In some implementations, separate compressor/turbine sets or pairs may advantageously be used in pumped thermal systems used with intermittent and/or variable electric power inputs. For example, a first compressor/turbine set can be used in a charge cycle that follows wind and/or solar power (e.g., electric power input from wind and/or solar power systems) while a second compressor/turbine set can be used in a discharge cycle that follows load (e.g., electric power output to a power grid). In this configuration, pumped thermal systems placed between a power generation system and a load may aid in smoothing variations/fluctuations in input and/or output power requirements.

Hybrid Pumped Thermal Systems

In accordance with another aspect of the disclosure, pumped thermal systems can be augmented by additional energy conversion processes and/or be directly utilized as energy conversion systems without energy storage (i.e., as power generation systems). In some examples, pumped thermal systems herein can be modified to allow for direct power generation using natural gas, Diesel fuel, petroleum gas (e.g., propane/butane), dimethyl ether, fuel oil, wood chips, landfill gas, hexane, hydrocarbons or any other combustible substance (e.g., fossil fuel or biomass) for adding heat to the working fluid on a hot side of a working fluid cycle, and a cold side heat sink (e.g., water) for removing heat from the working fluid on a cold side of the working fluid cycle.

FIGS. 24 and 25 show pumped thermal systems configured in generation mode. In some examples, pumped thermal systems herein can be modified by adding two additional heat exchangers 40 and 41, four additional valves 19 a, 19 b, 19 c and 19 d, a heat sink (e.g., a water cooling system; water from a fresh water reservoir such as a river, a lake or a reservoir; salt water from a salt water reservoir such as a sea or an ocean; air cooling using radiators, fans/blowers, convection; or an environmental heat sink such as ground/soil, cold air etc.) 42, and a heat source (e.g., a combustion chamber with a fuel-oxidant mixture) 43. The heat source 43 can exchange heat with a first of the two additional heat exchangers 40, and the heat sink 42 can exchange heat with a second of the two additional heat exchangers 41. The heat source 43 may be used to for exchanging heat with the working fluid 20.

The heat source 43 may be a combustion heat source. In some examples, the combustion heat source can comprise a combustion chamber for combusting a combustible substance (e.g., a fossil fuel, a synthetic fuel, municipal solid waste (MSW) or biomass). In some cases, the combustion chamber may be separate from the heat exchanger 40. In some cases, the heat exchanger 40 may comprise the combustion chamber. The heat source 43 may be a waste heat source, such as, for example waste heat from a power plant, an industrial process (e.g., furnace exhaust).

In some examples, a solar heater, a combustion heat source, a waste heat source, or any combination thereof may be used for heating the hot side heat storage fluid and/or the working fluid. In an example, the working fluid can be heated directly using any of these heat sources. In another example, the hot side heat storage fluid (or HTS medium) can be heated using any of these heat sources. In another example, the hot side heat storage fluid (or HTS medium) can be heated in parallel with the working fluid using any of these heat sources.

The pumped thermal systems in FIGS. 24 and 25 may be operated as hybrid systems. For example, the valves 19 a, 19 b, 19 c and 19 d can be used to switch between two modes. When the valves are in a first position, the system can operate as a pumped thermal storage system (e.g., closed system in charge/discharge mode). In this configuration, the working fluid 20 (e.g., argon or air) can exchange heat with an HTS medium (e.g., molten salt) in the hot side heat exchanger 2 and with a CTS medium (e.g., hexane) in the cold side heat exchanger 4. When the valves are in a second position, the system can operate as a power generation system (e.g., open system in generation mode). In this configuration, the heat exchangers 2 and 4 may be bypassed, and the working fluid 20 can exchange heat with the combustion chamber 43 in the hot side heat exchanger 40 and with the heat sink 42 in the cold side heat exchanger 41. Any description of configuration and/or design of heat transfer processes (e.g., heat transfer in heat exchangers) described herein in relation to pumped thermal systems may also be applied to hybrid pumped thermal systems, and vice versa. For example, the heat sink 42, the heat source 43, the heat exchangers 40 and 41, and/or the quantity of heat transferred on the cold side and/or the hot side may be configured to decrease or minimize entropy generation associated with heat transfer processes and/or to maximize system efficiency.

In some implementations, the hybrid systems may operate in storage and generation modes simultaneously. For example, the valves 19 a, 19 b, 19 c and 19 d can be configured to allow a given split between a working fluid flow rate to the heat exchangers 40 and 41 and a working fluid flow rate to the heat exchangers 2 and 4. Alternatively, the hybrid systems may operate exclusively in storage mode, or exclusively in generation mode (e.g., as a natural gas peaking plant). In some cases, the split between modes may be selected based on system efficiency, available electric power input (e.g., based on availability), desired electric power output (e.g., based on load demand) etc. For example, thermal efficiency of an ideal system (i.e., assuming isentropic compression and expansion processes, ideal heat transfer processes) operating exclusively in generation mode can be the thermal efficiency of a working fluid undergoing an ideal Brayton cycle. In some examples, thermal efficiencies in hybrid systems of the disclosure (e.g., exclusive and/or split mode operation) can be at least about 10%, at least about 20%, at least about 30%, at least about 40%, at least about 50%, at least about 60%, or more.

The heat source 43 may be used for exchanging heat with an HTS medium (e.g., a molten salt). For example, the combustion heat source 43 may be used for heating the HTS medium 21. In some instances, rather than using the combustion heat source 43 for exchanging heat in the heat exchanger 40 or for directly exchanging heat between flue gases from the combustion heat source and the working fluid, the combustion heat source 43 may be used to heat up the HTS medium 21 between the two HTS tanks 7 and 6.

FIG. 26 is a schematic flow diagram of hot side recharging in a pumped heat cycle through heating by the heat source 43 (e.g., combustion heat source, waste heat source). In an example, the heat source 43 is a waste heat source, such as a waste heat source from a refinery or other processing plant. In an example, the heat source 43 is obtained from combusting natural gas in order to ensure the delivery of electricity even if the pumped thermal system runs out of charged storage media. For example, recharging of the hot side storage media using the heat source 43 may provide an advantage over recharging using electricity or other means (e.g., the price of electricity at the time may be too high). The heat source 43 can be used to heat up the HTS medium 21 from the temperature T₁ in the tank 7 to the temperature T₁ ⁺ in the tank 6. The HTS medium can then be used in the CFX 2 for exchanging heat with the working fluid to in a discharge cycle, such as, for example, the discharge cycles in FIGS. 20 and 21.

In some examples, such as, for example, when the CTS medium is a combustible substance such as a fossil fuel (e.g., hexane or heptanes), burning of the CTS medium stored in the CTS tanks (e.g., the tanks 8 and 9) may be used for providing thermal energy for heating the HTS medium as shown, for example, in FIG. 26 or for operation of the cycles in the configurations shown, for example, in FIGS. 24 and 25.

The systems of the disclosure may be capable of operating both in an electricity only storage cycle (comprising heat transfer with an HTS medium and a CTS medium below ambient temperature) and in a heat engine to ambient cycle, where, in a discharge mode, heat is input from the HTS medium to the working fluid and rejected to the ambient environment rather than to the CTS medium. This capability may enable the use of heating of the HTS with combustible substances (e.g., as shown in FIG. 26) or the use of solar heating of the HTS (e.g., as shown in FIG. 19). Heat rejection to ambient may be implemented using, for example, the discharge cycles in FIGS. 20 and 21. In some cases, heat may be rejected to the environment with the aid of the ITS medium 61 or the intermediate medium 62.

Aspects of the disclosure may be synergistically combined. For example, the systems capable of operating both in an electricity only storage cycle and in a heat engine to ambient cycle may comprise a recuperator. Any description in relation to such hybrid systems without a recuperator may readily be applied to hybrid systems with a recuperator at least in some configurations. In some instances, the hybrid systems may be implemented using, for example, the parallel, valved configuration in FIG. 24. For example, the counter-flow heat exchangers 4 in FIGS. 20 and 21 may be implemented as separate counter-flow heat exchangers 67 for exchanging heat with the ambient environment, and may be used in combination with cold side counter-flow heat exchangers 4 of the disclosure.

In some implementations, the systems herein may be configured to enable switching between different cycles of the disclosure using a shared set of valves and pipes. For example, the system may be configured to switch between the electricity only charge cycle (such as shown in, for example, FIG. 15), the electricity only discharge cycle (such as shown in, for example, FIG. 16), and the heat engine to ambient cycle (such as shown in FIG. 21).

Pumped Thermal Systems with Pressure Regulation Power Control

In an aspect of the disclosure, the pressure of working fluids in pumped thermal systems can be controlled to achieve power control. In an example, the power provided to a closed system in charge mode and/or the power extracted from the closed system in discharge and/or generation mode (e.g., work input/output using the shaft 10) is proportional to the molar or mass flow rate of the circulating working fluid. The mass flow rate is proportional to density, area, and flow velocity. The flow velocity can be kept fixed in order to achieve a fixed shaft speed (e.g., 3600 rpm or 3000 rpm in accordance with power grid requirements of 60 and 50 Hz respectively). Thus, as the pressure of the working fluid changes, the mass flow rate and the power can change. In an example, as the mass flow rate increases in a discharge and/or generation mode, more load should be added to the system to maintain a constant speed of the rotating shaft, and vice versa. In another example, if load is reduced during operation in a discharge and/or generation mode, the reduced load can cause the shaft speed to increase, thus increasing the mass flow rate. For some period of time, before the heat stored in the thermal capacity of the heat exchangers themselves is dissipated, this increased mass flow rate can lead to an increase in the power delivered, in turn increasing the shaft speed. The shaft speed and the power can continue to increase uncontrollably, resulting in a runaway of the rotating shaft. In some examples, pressure regulation may enable control, and thus stabilization of runaway, through adjustment of the amount (e.g., density) of circulating working fluid in accordance with system requirements. In an example where shaft speed (and turbomachinery, such as a turbine, attached to the shaft) begins to run away, a controller can reduce the mass of circulating working fluid (e.g., mass flow rate) in order to decrease the power delivered, in turn decreasing the shaft speed. Pressure regulation may also allow for an increase in mass flow rate in response to an increase in load. In each of these instances, the flow rates of the HTS and CTS media through the heat exchangers can be matched to the heat capacity of the working fluid passing through the heat exchangers.

In some examples, the working fluid pressure in the closed system can be varied by using an auxiliary working fluid tank in fluid communication with the closed system. In this configuration, power input/output can be decreased by transferring the working fluid from the closed cycle loop to the tank, and power input/output can be increased by transferring the working fluid from the tank to the closed cycle loop. In an example, when the pressure of the working fluid is decreased, less heat can be transferred between the thermal storage tanks on the hot and cold sides of the system as a result of the decreased mass flow rate and less power can be input to/output by the system.

As the pressure of the working fluid is varied, the compression ratios of turbomachinery components may remain substantially unchanged. In some cases, one or more operating parameters and/or configuration (e.g., variable stators, shaft speed) of turbomachinery components can be adjusted in response to a change in working fluid pressure (e.g., to achieve a desired performance of the system). Alternatively, one or more pressure ratios may change in response to a change in working fluid pressure.

In some cases, reduced cost and/or reduced parasitic energy consumption may be achieved using the power control configuration relative to other configurations (e.g., using a choke valve for controlling the flow of the working fluid). In some examples, variation of working fluid pressure while keeping the temperature and flow velocity constant (or near-constant) may lead to negligible entropy generation. In some examples, an increase or decrease in system pressure may lead to changes in, for example, turbomachinery efficiencies.

FIG. 27 shows an example of a pumped thermal system with power control. The temperature of the working fluid on the hot and cold sides of the system may remain constant or near-constant for a given period of time regardless of working fluid mass flow rate due to large heat capacities of the heat exchangers 2 and 4 and/or the hot and cold side thermal storage media in the tanks 6, 7, 8 and 9. In some examples, the flow rates of the HTS and CTS media through the heat exchangers 2 and 4 are varied in concert with a change in the pressure of the working fluid in order to keep the temperatures in the heat exchangers and working fluid optimized over longer time periods. Thus, pressure can be used to vary the mass flow rate in the system. One or more auxiliary tanks 44 filled with the working fluid 20 (e.g., air, argon or argon-helium mix) can be in fluid communication with a hot (e.g., high pressure) side of the pumped thermal system and/or a cold (e.g., low pressure) side of the pumped thermal system. In some examples, the auxiliary tank can be in fluid communication with the working fluid adjacent to an inlet of the compressor 1 and/or adjacent to an outlet of the compressor 1. In some examples, the auxiliary tank can be in fluid communication with the working fluid adjacent to an inlet of the turbine 3 and/or adjacent to an outlet of the turbine 3. In further examples, the auxiliary tank can be in fluid communication with the working fluid in one or more locations system (e.g., one or more locations on the high pressure side of the system, on the low pressure side of the system, or any combination thereof). For example, the auxiliary tank can be in fluid communication with the working fluid on a high pressure side and a low pressure side of the closed cycle. In some cases, the fluid communication on the high pressure side can be provided after the compressor and before the turbine. In some cases, the fluid communication on the low pressure side can be provided after the turbine and before the compressor. In some instances, the auxiliary tank can contain working fluid at a pressure intermediate to the high and low pressures of the system. The working fluid in the auxiliary tank can be used to increase or decrease the amount of working fluid 20 circulating in the closed cycle of the pumped thermal system. The amount of working fluid circulating in the closed cycle loop can be decreased by bleeding the working fluid from the high pressure side of the closed cycle loop into the tank through a fluid path containing a valve or mass flow controller 46, thereby charging the tank 44. The amount of working fluid circulating in the closed cycle loop can be increased by bleeding the working fluid from the tank into the low pressure side of the closed cycle loop through a fluid path containing a valve or mass flow controller 45, thereby discharging the tank 44.

Power control over longer timescales may be implemented by changing the pressure of the working fluid and by adjusting the flow rates of the hot side 21 and cold side 22 thermal storage fluids through the heat exchangers 2 and 4, respectively.

In some examples, flow rates of the thermal storage media 21 and/or 22 may be controlled (e.g., by a controller) to maintain given heat exchanger inlet and outlet temperatures. In some examples, a first controller(s) may be provided for controlling the flow rates (e.g., mass flow rates) of thermal storage media, and a second controller may be provided for controlling the mass flow rate (e.g., by controlling mass, mass flow rate, pressure etc.) of the working fluid.

Pumped Thermal Systems with Pressure-Encased Motor/Generator

In another aspect of the disclosure, pumped thermal systems with a pressure-encased motor/generator are provided. The pressure-encased motor/generator may be provided as an alternative to configurations where a shaft (also “crankshaft” herein) penetrates through a working fluid containment wall (where it can be exposed to one or more relatively high pressure differentials) in order to connect to a motor/generator outside the working fluid containment wall. In some cases, the shaft may be exposed to pressures and temperatures of the working fluid in the low pressure portion of the working fluid cycle, in the high pressure portion of the working fluid cycle, or both. In some cases, crankshaft seal(s) capable of holding back the pressures which the crankshaft is exposed to inside the working fluid containment wall can be difficult to manufacture and/or difficult to maintain. In some cases, a rotating seal between high and low pressure environments may be difficult to achieve. Thus, coupling of the compressor and turbine to the motor/generator can be challenging. In some implementations, the motor/generator can therefore be placed entirely within the low pressure portion of the working fluid cycle, such that the exterior pressure vessel or working fluid containment wall may not need to be penetrated.

FIG. 28 shows an example of a pumped thermal system with a pressure encased generator 11. The motor/generator is encased within the pressure vessel or working fluid containment wall (shown as dashed lines) and only feed-through electric leads 49 penetrate through the pressure vessel. A thermal insulation wall 48 is added between the motor/generator 11 and the working fluid in the low pressure portion of the cycle. The technical requirements for achieving an adequate seal through the thermal insulation wall can be less stringent due to the pressure being the same on both sides of the thermal insulation wall (e.g., both sides of the thermal insulation wall can be located in the low pressure portion of the cycle). In an example, the low pressure value can be about 10 atm. In some cases, the motor/generator may be adapted for operation at elevated surrounding pressures. An additional thermal insulation wall 50 can be used to create a seal between the outlet of the compressor 1 and the inlet of the turbine 3 in the high pressure portion of the cycle. In some examples, placing the motor/generator on the cold side of the pumped thermal systems may be beneficial to the operation of the motor/generator (e.g., cooling of a superconducting generator).

Pumped Thermal Systems with Variable Stator Pressure Ratio Control

A further aspect of the disclosure relates to control of pressure in working fluid cycles of pumped thermal systems by using variable stators. In some examples, use of variable stators in turbomachinery components can allow pressure ratios in working fluid cycles to be varied. The variable compression ratio can be accomplished by having movable stators in the turbomachinery.

In some cases, pumped thermal systems (e.g., the systems in FIGS. 17 and 18) can operate at the same compression ratio in both the charge and the discharge cycles. In this configuration, heat can be rejected (e.g., to the environment) in section 38 in the charge cycle and in section 39 in the discharge cycle, wherein the heat in section 38 can be transferred at a lower temperature than the heat in section 39. In alternative configurations, the compression ratio can be varied when switching between the charge cycle and the discharge cycle. In an example, variable stators can be added to both the compressor and the turbine, thus allowing the compression ratio to be tuned. The ability to vary compression ratio between charge and discharge modes may enable heat to be rejected at the lower temperature only (e.g., heat may be rejected in section 38 in the charge cycle but not in section 39 in the discharge cycle). In some examples, a greater portion (or all) of the heat rejected to the environment is transferred at a lower temperature, which may increase the roundtrip efficiency of the system.

FIG. 29 is an example of variable stators in a compressor/turbine pair. The compressor 1 and the turbine 3 can both have variable stators, so that the compression ratio for each can be tuned. Such tuning may increase roundtrip efficiency.

The compressor and/or the turbine can (each) include one or more compression stages. For example, the compressor and/or the turbine can have multiple rows of repeating features distributed along its circumference. Each compression stage can comprise one or more rows of features. The rows may be arranged in a given order. In one example, the compressor 1 and the turbine 3 each comprise a sequence of a plurality of inlet guide vanes 51, a first plurality of rotors 52, a plurality of stators 53, a second plurality of rotors 52 and a plurality of outlet guide vanes 54. Each plurality of features can be arranged in a row along the circumference of the compressor/turbine. The configuration (e.g., direction or angle) of the stators 53 can be varied, as indicated in FIG. 29.

The compressor/turbine pair can be matched. In some cases, an outlet pressure of the compressor can be about the same as an inlet pressure of the turbine, and an inlet pressure of the compressor can be about the same as the outlet pressure of the turbine; thus, the pressure ratio across the turbine can be the same as the pressure ratio across the compressor. In some cases, the inlet/outlet pressures and/or the pressure ratios may differ by a given amount (e.g., to account for pressure drop in the system). The use of variable stators on both the compressor and the turbine can allow the compressor and the turbine to remain matched as the compression ratio is varied. For example, using the variable stators, operation of the compressor and the turbine can remain within suitable operating conditions (e.g. within a given range or at a given point on their respective operating maps) as the compression ratio is varied. Operation within given ranges or at given points on turbomachinery operating maps may allow turbomachinery efficiencies (e.g., isentropic efficiencies) and resulting roundtrip storage efficiency to be maintained within a desired range. In some implementations, the use of variable stators can be combined with other methods for varying the compression ratios (e.g. variable shaft rotation speed, bypassing of turbomachinery stages, gears, power electronics, etc.).

Pumped Thermal System Units Comprising Pumped Thermal System Subunits

A further aspect of the disclosure relates to control of charging and discharging rate over a full range from maximum charging/power input to maximum discharging/power output by building composite pumped thermal system units comprised of pumped thermal system subunits. In some examples, pumped thermal systems may have a minimum power input and/or output (e.g., minimum power input and/or minimum power output) above 0% of maximum power input and/or output (e.g., maximum power input and/or maximum power output), respectively. In such cases, a single unit by itself may be able to continuously ramp from the minimum power input to the maximum power input and from the minimum power output to the maximum power output, but may not be able to continuously ramp from the minimum power input to the minimum power output (i.e., maximum the minimum power input to zero power input/output, and from zero power input/output to the minimum power output). An ability to continuously ramp from the minimum power input to the minimum power output may enable the system to continuously ramp from the maximum power input to the maximum power output. For example, if both the output power and the input power may be turned down all the way to zero during operation, the system may be able to continuously vary the power consumed or supplied across a range from the maximum input (e.g., acting as a load on the grid) to the maximum output (e.g., acting as a generator on the grid). Such functionality may increase (e.g., more than double) the continuously rampable range of the pumped thermal system. Increasing the continuously rampable range of the pumped thermal system may be advantageous, for example, when continuously rampable power range is used as a metric for determining the value of grid assets. Further, such functionality may enable the systems of the disclosure to follow variable load, variable generation, intermittent generation, or any combination thereof.

In some implementations, composite pumped thermal system units comprised of multiple pumped thermal system subunits may be used. In some cases, each subunit may have a minimum power input and/or output above 0%. The continuous ramping of the power from the maximum power input to the maximum power output may include combining a given quantity of the subunits. For example, a suitable (e.g., sufficiently large) number of subunits may be needed to achieve continuous ramping. In some examples, the number of subunits can be at least about 2, 5, 10, 20, 30, 40, 50, 100, 200, 500, 750, 1000, and the like. In some examples, the number of subunits is 2, 5, 10, 20, 30, 40, 50, 100, 150, 200, 250, 300, 350, 400, 450, 500, 550, 600, 650, 700, 750, 800, 850, 900, 950, 1000 or more. Each subunit may have a given power capacity. For example, each subunit can have a power capacity that is less than about 0.1%, less than about 0.5%, less than about 1%, less than about 5%, less than about 10%, less than about 25%, less than about 50%, or less than about 90% of the total power capacity of the composite pumped thermal system. In some cases, different subunits may have different power capacities. In some examples, a subunit has a power capacity of about 10 kW, 100 kW, 500 kW, 1 MW, 2 MW, 5 MW, 10 MW, 20 MW, 50 MW, 100 MW, or more. The continuous ramping of the power from the maximum power input to the maximum power output may include controlling each subunit's power input and/or output (e.g., power input and/or power output) separately. In some cases, the subunits may be operated in opposing directions (e.g., one or more subunits may operate in power input mode while one or more subunits may operate in power output mode). In one example, if each pumped thermal system subunit can be continuously ramped between a maximum power input and/or output down to about 50% of the maximum power input and/or output, respectively, three or more such pumped thermal system subunits may be combined into a composite pumped thermal system unit that can be continuously ramped from the maximum input power to the maximum output power. In some implementations, the composite pumped thermal system may not have a fully continuous range between the maximum input power and the maximum output power, but may have an increased number of operating points in this range compared to a non-composite system.

Energy Storage System Units Comprising Energy Storage System Subunits

A further aspect of the disclosure relates to control of charging and discharging rate over a full range from maximum charging/power input to maximum discharging/power output by building composite energy storage system units comprised of energy storage system subunits. In some examples, energy storage systems may have a minimum power input and/or output (e.g., minimum power input and/or minimum power output) above 0% of maximum power input and/or output (e.g., maximum power input and/or maximum power output), respectively. In such cases, a single unit by itself may be able to continuously ramp from the minimum power input to the maximum power input and from the minimum power output to the maximum power output, but may not be able to continuously ramp from the minimum power input to the minimum power output (i.e., from the minimum power input to zero power input/output, and from zero power input/output to the minimum power output). An ability to continuously ramp from the minimum power input to the minimum power output may enable the system to continuously ramp from the maximum power input to the maximum power output. For example, if both the output power and the input power may be turned down all the way to zero during operation, the system may be able to continuously vary the power consumed or supplied across a range from the maximum input (e.g., acting as a load on the grid) to the maximum output (e.g., acting as a generator on the grid). Such functionality may increase (e.g., more than double) the continuously rampable range of the energy storage system. Increasing the continuously rampable range of the energy storage system may be advantageous, for example, when continuously rampable power range is used as a metric for determining the value of grid assets. Further, such functionality may enable the systems of the disclosure to follow variable load, variable generation, intermittent generation, or any combination thereof.

In some implementations, composite energy storage system units comprised of multiple energy storage system subunits may be used. In some examples, any energy storage system having power input/output characteristics that may benefit from a composite configuration may be used. In some examples, systems having power input and/or power output characteristics that may benefit from a composite configuration may include various power storage and/or generation systems such as, for example, natural gas or combined cycle power plants, fuel cell systems, battery systems, compressed air energy storage systems, pumped hydroelectric systems, etc. In some cases, each subunit may have a minimum power input and/or output above 0%. The continuous ramping of the power from the maximum power input to the maximum power output may include combining a given quantity of the subunits. For example, a suitable (e.g., sufficiently large) number of subunits may be needed to achieve continuous ramping. In some examples, the number of subunits can be at least about 2, 5, 10, 20, 30, 40, 50, 100, 200, 500, 750, 1000, and the like. In some examples, the number of subunits is 2, 5, 10, 20, 30, 40, 50, 100, 150, 200, 250, 300, 350, 400, 450, 500, 550, 600, 650, 700, 750, 800, 850, 900, 950, 1000 or more. Each subunit may have a given power capacity. For example, each subunit can have a power capacity that is less than about 0.1%, less than about 0.5%, less than about 1%, less than about 5%, less than about 10%, less than about 25%, less than about 50%, or less than about 90% of the total power capacity of the composite energy storage system. In some cases, different subunits may have different power capacities. In some examples, a subunit has a power capacity of about 10 kW, 100 kW, 500 kW, 1 MW, 2 MW, 5 MW, 10 MW, 20 MW, 50 MW, 100 MW, or more. The continuous ramping of the power from the maximum power input to the maximum power output may include controlling each subunit's power input and/or output (e.g., power input and/or power output) separately. In some cases, the subunits may be operated in opposing directions (e.g., one or more subunits may operate in power input mode while one or more subunits may operate in power output mode). In one example, if each energy storage system subunit can be continuously ramped between a maximum power input and/or output down to about 50% of the maximum power input and/or output, respectively, three or more such energy storage system subunits may be combined into a composite energy storage system unit that can be continuously ramped from the maximum input power to the maximum output power. In some implementations, the composite energy storage system may not have a fully continuous range between the maximum input power and the maximum output power, but may have an increased number of operating points in this range compared to a non-composite system.

Control Systems

The present disclosure provides computer control systems (or controllers) that are programmed to implement methods of the disclosure. FIG. 30 shows a computer system 1901 (or controller) that is programmed or otherwise configured to regulate various process parameters of energy storage and/or retrieval systems disclosed herein. Such process parameters can include temperatures, flow rates, pressures and entropy changes.

The computer system 1901 includes a central processing unit (CPU, also “processor” and “computer processor” herein) 1905, which can be a single core or multi core processor, or a plurality of processors for parallel processing. The computer system 1901 also includes memory or memory location 1910 (e.g., random-access memory, read-only memory, flash memory), electronic storage unit 1915 (e.g., hard disk), communication interface 1920 (e.g., network adapter) for communicating with one or more other systems, and peripheral devices 1925, such as cache, other memory, data storage and/or electronic display adapters. The memory 1910, storage unit 1915, interface 1920 and peripheral devices 1925 are in communication with the CPU 1905 through a communication bus (solid lines), such as a motherboard. The storage unit 1915 can be a data storage unit (or data repository) for storing data. The computer system 1901 can be operatively coupled to a computer network (“network”) 1930 with the aid of the communication interface 1920. The network 1930 can be the Internet, an internet and/or extranet, or an intranet and/or extranet that is in communication with the Internet. The network 1930 in some cases is a telecommunication and/or data network. The network 1930 can include one or more computer servers, which can enable distributed computing, such as cloud computing. The network 1930, in some cases with the aid of the computer system 1901, can implement a peer-to-peer network, which may enable devices coupled to the computer system 1901 to behave as a client or a server.

The computer system 1901 is coupled to an energy storage and/or retrieval system 1935, which can be as described above or elsewhere herein. The computer system 1901 can be coupled to various unit operations of the system 1935, such as flow regulators (e.g., valves), temperature sensors, pressure sensors, compressor(s), turbine(s), electrical switches, and photovoltaic modules. The system 1901 can be directly coupled to, or be a part of, the system 1935, or be in communication with the system 1935 through the network 1930.

The CPU 1905 can execute a sequence of machine-readable instructions, which can be embodied in a program or software. The instructions may be stored in a memory location, such as the memory 1910. Examples of operations performed by the CPU 1905 can include fetch, decode, execute, and writeback.

With continued reference to FIG. 30, the storage unit 1915 can store files, such as drivers, libraries and saved programs. The storage unit 1915 can store programs generated by users and recorded sessions, as well as output(s) associated with the programs. The storage unit 1915 can store user data, e.g., user preferences and user programs. The computer system 1901 in some cases can include one or more additional data storage units that are external to the computer system 1901, such as located on a remote server that is in communication with the computer system 1901 through an intranet or the Internet.

The computer system 1901 can communicate with one or more remote computer systems through the network 1930. For instance, the computer system 1901 can communicate with a remote computer system of a user (e.g., operator). Examples of remote computer systems include personal computers, slate or tablet PC's, telephones, Smart phones, or personal digital assistants. The user can access the computer system 1901 via the network 1930.

Methods as described herein can be implemented by way of machine (e.g., computer processor) executable code stored on an electronic storage location of the computer system 1901, such as, for example, on the memory 1910 or electronic storage unit 1915. The machine executable or machine readable code can be provided in the form of software. During use, the code can be executed by the processor 1905. In some cases, the code can be retrieved from the storage unit 1915 and stored on the memory 1910 for ready access by the processor 1905. In some situations, the electronic storage unit 1915 can be precluded, and machine-executable instructions are stored on memory 1910.

The code can be pre-compiled and configured for use with a machine have a processor adapted to execute the code, or can be compiled during runtime. The code can be supplied in a programming language that can be selected to enable the code to execute in a pre-compiled or as-compiled fashion.

Aspects of the systems and methods provided herein, such as the computer system 1901, can be embodied in programming. Various aspects of the technology may be thought of as “products” or “articles of manufacture” typically in the form of machine (or processor) executable code and/or associated data that is carried on or embodied in a type of machine readable medium. Machine-executable code can be stored on an electronic storage unit, such memory (e.g., read-only memory, random-access memory, flash memory) or a hard disk. “Storage” type media can include any or all of the tangible memory of the computers, processors or the like, or associated modules thereof, such as various semiconductor memories, tape drives, disk drives and the like, which may provide non-transitory storage at any time for the software programming. All or portions of the software may at times be communicated through the Internet or various other telecommunication networks. Such communications, for example, may enable loading of the software from one computer or processor into another, for example, from a management server or host computer into the computer platform of an application server. Thus, another type of media that may bear the software elements includes optical, electrical and electromagnetic waves, such as used across physical interfaces between local devices, through wired and optical landline networks and over various air-links. The physical elements that carry such waves, such as wired or wireless links, optical links or the like, also may be considered as media bearing the software. As used herein, unless restricted to non-transitory, tangible “storage” media, terms such as computer or machine “readable medium” refer to any medium that participates in providing instructions to a processor for execution.

Hence, a machine readable medium, such as computer-executable code, may take many forms, including but not limited to, a tangible storage medium, a carrier wave medium or physical transmission medium. Non-volatile storage media include, for example, optical or magnetic disks, such as any of the storage devices in any computer(s) or the like, such as may be used to implement the databases, etc. shown in the drawings. Volatile storage media include dynamic memory, such as main memory of such a computer platform. Tangible transmission media include coaxial cables; copper wire and fiber optics, including the wires that comprise a bus within a computer system. Carrier-wave transmission media may take the form of electric or electromagnetic signals, or acoustic or light waves such as those generated during radio frequency (RF) and infrared (IR) data communications. Common forms of computer-readable media therefore include for example: a floppy disk, a flexible disk, hard disk, magnetic tape, any other magnetic medium, a CD-ROM, DVD or DVD-ROM, any other optical medium, punch cards paper tape, any other physical storage medium with patterns of holes, a RAM, a ROM, a PROM and EPROM, a FLASH-EPROM, any other memory chip or cartridge, a carrier wave transporting data or instructions, cables or links transporting such a carrier wave, or any other medium from which a computer may read programming code and/or data. Many of these forms of computer readable media may be involved in carrying one or more sequences of one or more instructions to a processor for execution.

III. ILLUSTRATIVE COLD SIDE HEAT DISSIPATION

In one embodiment, charge and discharge cycles of a closed cycle system, such as a Brayton cycle energy storage and power generation system, may defined by the Pressure-Temperature charts illustrated in FIGS. 31 and 32, respectively. If polytropic efficiencies of turbomachinery in the embodiment are less than 100%, and if T₀, T₁, and T₁ ⁺ are kept constant between charge and discharge cycles, then T₀ ^(+(d))>T₀ ^(+(c)) and the excess heat may need to be dissipated between the discharge and charge cycle.

FIGS. 33 and 34 illustrate embodiments of example Brayton systems in discharge mode with cold side heat storage that may be used to dissipate the excess heat described above. The embodiments are illustrative examples only and the cold side heat storage may be implemented in other Brayton systems, including those disclosed herein. The systems in FIGS. 33 and 34 include a working fluid 120 flowing through at least, in sequence, a compressor 101, a recuperator 105, a hot side heat exchanger 102, a turbine 103, and a cold side heat exchanger 104. A hot side thermal storage (“HTS”) medium 121 may flow from HTS tank 106, through hot side heat exchanger 102, and to HTS tank 107. A CTS medium 122 may flow through the cold side heat exchanger 104 and between two or more tanks. Fluid paths are as indicated in individual Figures and flow direction of a fluid in a given fluid path are indicated by one or more arrows. Each of the above identified fluids, components, and/or fluid paths may be the same or similar to previously described closed cycle elements (e.g., Brayton cycle elements), such as working fluid 20, compressor 1, recuperator 5, hot side heat exchanger 2, turbine 3, cold side heat exchanger 4, HTS medium 21, HTS tank 6, HTS tank 7, and CTS medium 122. Additionally, CTS tanks 108 and 109 may be the same or similar to CTS tanks 8 and 9. FIGS. 33 and 34 are illustrative only and other fluids, components and/or fluid paths may be present. Some components, such as a hot side or cold side heat exchangers or tanks may be replaced with other components that serve a similar thermal purpose.

In FIG. 33, a working fluid may circulate in a closed cycle path through at least, in sequence, the compressor 101, the recuperator 105, the hot side heat exchanger 102, the turbine 103, the recuperator 105, a cooling heat exchanger 150, and the cold side heat exchanger 104. The cooling heat exchanger 105 is configured to remove heat from the working fluid 120.

Cooling heat exchanger 150 may expel excess heat stored in the working fluid 120 on the cold side of the system. In one embodiment, cooling heat exchanger 150 may act as a radiator and expel heat directly to the ambient environment; however, this may be impractical if the working fluid 120 entering the cooling heat exchanger 150 is near ambient temperature. In another embodiment, a thermal fluid 155 may circulate between the cooling heat exchanger 150 and a heat sink 151. The thermal fluid may be, for example, water or another fluid such as Therminol®. The heat sink 151 may be, as non-limiting examples, a cooling tower, an air cooling heat exchanger, or an environmental heat sink.

In FIG. 34, a working fluid 120 may circulate in a closed cycle path through at least, in sequence, the compressor 101, the recuperator 105, the hot side heat exchanger 102, the turbine 103, the recuperator 105, and the cold side heat exchanger 104. A CTS medium 122 may flow from CTS tank 109 through cold side heat exchanger 104 and to an intermediate tank 152. To store excess heat from the Brayton cycle, the CTS medium 122 may be allowed to heat up to a higher temperature during the discharge cycle than is needed on input to a charge cycle. This “hotter” CTS medium 122 may then flow to a CTS heat exchanger 153 where it is cooled to a temperature appropriate for use in a charge cycle and store in CTS tank 108. CTS heat exchanger 153 may be, as non-limiting examples, a cooling tower, an air cooling heat exchanger, or an environmental heat sink.

As a specific example, a notional Brayton system discharge cycle is defined in which the working fluid is air, the HTS medium 121 is molten salt operating between 565° C. and 290° C., and the CTS medium 122 is hexane, which would normally operate between −60° and 35°. Due to inefficiencies or intentional operational reasons, the CTS medium 122 may be allowed to enter the cold side heat exchanger at >35°. This “hotter” CTS medium 122 may be dumped to the intermediate tank 152 and cooled over time to ˜35° C. through the CTS heat exchanger 153, before being finally stored in the CTS tank 108, ready for re-use in a charging cycle. A variable flow rate may be used in the fluid path between intermediate tank 152 and CTS tank 108 in order to take advantage of a longer cooling cycle through the CTS heat exchanger 153.

In some embodiments, so much excess heat may be carried into the cold side that the CTS medium 122 may reach its boiling point. As a specific example, the boiling point of hexane at ambient pressure is 68° C. In one embodiment, the CTS medium 122 may be allowed to evaporate, taking advantage of its latent heat of vaporization and then re-condensed. However, this may carry some additional costs for gas handling infrastructure. In another embodiment, the flow of CTS medium 122 through the cold side heat exchanger 104 may have a variable flowrate, which may be increased to provide additional cooling while keeping the temperature of the CTS medium 122 below its boiling point.

In another embodiment, the flow of CTS medium 122 through the cold side heat exchanger 104 be increased by augmenting the flow with CTS medium 122 from CTS tank 108. As shown by fluid path 154, CTS medium 122 from CTS tank 108 may enter the cold side heat exchanger 104 at some point intermediate to the inlet of “cold” CTS medium 122 from CTS tank 109 and the outlet of “hotter” CTS medium 122 to intermediate tank 152. By adjusting the flow rate in fluid path 154 and/or the entry point of fluid path 154 to the fluid path of CTS medium 122 through the cold side heat exchanger 104, the exit temperature of CTS medium 122 can be kept below its boiling point.

FIG. 35 illustrates a method 200 for storing and dissipating heat from cold side heat storage, according to an example embodiment. The embodiment is an illustrative example only and the cold side heat storage may be implemented in other Brayton systems, including those disclosed herein.

In step 202, in a Brayton cycle system operating in a power generation mode (discharge mode), a working fluid is circulated through a closed cycle fluid path including, in sequence, a compressor, a recuperator, a hot side heat exchanger, a turbine, the recuperator, and a cold side heat exchanger.

In step 204, a CTS medium is flowed at a first variable flow rate from a first CTS tank, through the cold side heat exchanger and in thermal contact with the working fluid, and to an intermediate CTS tank.

In step 206, the CTS medium from the intermediate CTS tank is flowed through a CTS heat exchanger, and to a second CTS tank, wherein the CTS heat exchanger is configured to remove heat from the CTS medium.

Additionally, the first variable flow rate may be varied based on a temperature of the CTS medium. As described above, the CTS medium may also be flowed at a second variable flow rate from the second tank to the cold side heat exchanger, and the second variable flow rate may be varied based on a temperature of the CTS medium.

IV. CONCLUSION

While various aspects and embodiments have been disclosed herein, other aspects and embodiments will be apparent to those skilled in the art. The various aspects and embodiments disclosed herein are for purposes of illustration and are not intended to be limiting, with the true scope and spirit being indicated by the following claims. 

1. A system comprising: a compressor; a recuperator; a hot side heat exchanger; a turbine; a cold side heat exchanger; a cooling heat exchanger; and a working fluid circulating in a closed cycle path through, in sequence, the compressor, the recuperator, the hot side heat exchanger, the turbine, the recuperator, the cooling heat exchanger, and the cold side heat exchanger in a discharge mode and the compressor, the hot-side heat exchanger, the recuperator, the turbine, the cold-side heat exchanger, and the recuperator in a charge mode, wherein the cooling heat exchanger is configured to remove heat from the working fluid.
 2. The system of claim 1, wherein the working fluid circulates in the closed cycle path in the same direction in both the charge mode and the discharge mode.
 3. The system of claim 1, further comprising: a first cold side thermal storage (“CTS”) tank; a second CTS tank; and a CTS medium flowing from the first CTS tank, through the cold side heat exchanger, and to the second CTS tank.
 4. The system of claim 3, further comprising: a first hot side thermal storage (“HTS”) tank; a second HTS tank; and an HTS medium flowing from the first HTS tank, through the hot side heat exchanger, and to the second HTS tank.
 5. The system of claim 4, wherein the HTS medium is molten salt.
 6. The system of claim 1, wherein the cooling heat exchanger is a radiator, wherein the working fluid circulating through the cooling heat exchanger expels heat to air.
 7. The system of claim 1, wherein the cooling heat exchanger circulates a thermal fluid in thermal contact with a heat sink.
 8. The system of claim 7, wherein the heat sink is a cooling tower.
 9. A system comprising: a compressor; a recuperator; a hot side heat exchanger; a turbine; a cold side heat exchanger; a working fluid circulating in a closed cycle path through, in sequence, the compressor, the recuperator, the hot side heat exchanger, the turbine, the recuperator, and the cold side heat exchanger in a discharge mode and the compressor, the hot-side heat exchanger, the recuperator, the turbine, the cold-side heat exchanger, and the recuperator in a charge mode; a cold side thermal storage (“CTS”) medium; a first CTS tank; an intermediate CTS tank; a CTS heat exchanger, wherein the CTS heat exchanger is configured to remove heat from the CTS medium; a second CTS tank; a first flow path configured to flow CTS medium from the first CTS tank, through the cold side heat exchanger, and to the intermediate CTS tank; and a second flow path configured to flow CTS medium from the intermediate CTS tank, through the CTS heat exchanger, and to the second CTS tank.
 10. The system of claim 9, wherein the working fluid circulates in the closed cycle path in the same direction in both the charge mode and the discharge mode.
 11. The system of claim 9, further comprising: a first hot side thermal storage (“HTS”) tank; a second HTS tank; and an HTS medium flowing from the first HTS tank, through the hot side heat exchanger, and to the second HTS tank.
 12. The system of claim 11, wherein the CTS heat exchanger is a cooling tower.
 13. The system of claim 11, wherein the CTS heat exchanger is a radiator, wherein the CTS medium flowing through the CTS heat exchanger expels heat to air.
 14. The system of claim 11, further comprising a third flow path configured to flow CTS medium from the second CTS tank to the first flow path and inject CTS medium from the second CTS tank into the first flow path.
 15. The system of claim 14, wherein the third flow path intersects the first flow path at a location intermediate to the first flow path entering the cold side heat exchanger and the first flow path exiting the cold side heat exchanger.
 16. A method comprising: in a closed cycle system operating in a power generation mode, circulating a working fluid through a closed cycle fluid path including, in sequence, a compressor, a recuperator, a hot side heat exchanger, a turbine, the recuperator, and a cold side heat exchanger in a discharge mode and the compressor, the hot-side heat exchanger, the recuperator, the turbine, the cold-side heat exchanger, and the recuperator in a charge mode; flowing a cold side thermal storage (“CTS”) medium at a first variable flow rate from a first CTS tank, through the cold side heat exchanger and in thermal contact with the working fluid, and to an intermediate CTS tank; and flowing the CTS medium from the intermediate CTS tank, through a CTS heat exchanger, and to a second CTS tank, wherein the CTS heat exchanger is configured to remove heat from the CTS medium.
 17. The system of claim 16, wherein the working fluid circulates in the closed cycle path in the same direction in both the charge mode and the discharge mode.
 18. The method of claim 16, further comprising varying the first variable flow rate based on a temperature of the CTS medium.
 19. The method of claim 18, further comprising flowing the CTS medium at a second variable flow rate from the second CTS tank to the cold side heat exchanger.
 20. The method of claim 19, further comprising varying the second variable flow rate based on a temperature of the CTS medium. 